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  <url>
    <loc>https://carolinekrawczyk.com/design-portfolio</loc>
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    <lastmod>2024-12-12</lastmod>
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      <image:title>Design Portfolio</image:title>
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      <image:title>Design Portfolio</image:title>
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  <url>
    <loc>https://carolinekrawczyk.com/engine-diffuser-seal</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-19</lastmod>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
      <image:caption>Chart compares cold temperature (orange) and room temperature (blue) data to develop shear buckling temperature knockdown</image:caption>
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    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616006660354-GQ0YXSUR98EYHM4QP0GV/engine+diffuser+seal+3.png</image:loc>
      <image:title>Engine Diffuser Seal</image:title>
      <image:caption>Scrappy Material Properties Testing for Engine Diffuser Seal</image:caption>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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      <image:title>Engine Diffuser Seal</image:title>
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    <image:image>
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      <image:title>Engine Diffuser Seal</image:title>
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    <image:image>
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      <image:title>Engine Diffuser Seal</image:title>
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    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/5ec321c2af33de48734cc929/1589847319534-81UFWBJ847PXRDO7CHWE/Large+JPG-Aro+Ha_0380.jpg</image:loc>
      <image:title>Engine Diffuser Seal</image:title>
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  </url>
  <url>
    <loc>https://carolinekrawczyk.com/contact</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2025-11-07</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/7d34e52f-073f-4cef-9341-440d4804e769/motorcycle+smile.jpg</image:loc>
      <image:title>Contact - Contact Me.</image:title>
      <image:caption>Email: CaroKrawczykConsulting@gmail.com Phone: +1 (224) 523-3585 LinkedIn</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/testing</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-19</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1612666103523-HVQ7M95EHY00V2HYC6E2/Risk%252BRedux%252BDuct%252B-%252BInlet%252BStructural%252BTesting.jpg</image:loc>
      <image:title>Testing</image:title>
      <image:caption>Core shear failure at core ramps predicted to occur at 9.5 psig</image:caption>
    </image:image>
    <image:image>
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      <image:title>Testing</image:title>
      <image:caption>Inlet Duct Testing Setup</image:caption>
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    <image:image>
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      <image:title>Testing</image:title>
      <image:caption>Took inlet duct to failure at 34 psig. Core shear is present in test article as shown in the picture above</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616181977439-XUL2V54Q81V4HUG5LIYX/nlg+drop+test+3.png</image:loc>
      <image:title>Testing</image:title>
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    <image:image>
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      <image:title>Testing</image:title>
      <image:caption>Blade seal shown in gold with yellow flight tag. Test conducted in an afternoon to get quick results to inform aircraft build.</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/xb-1-outboard-inlets</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-23</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614697167598-968G4F2479FY6WCUM9TT/ob%2Binlet%2B8%2Bwind%2Btunnel.jpg</image:loc>
      <image:title>XB-1 Outboard Inlets - High-Efficiency Aerodynamic Surfacing</image:title>
      <image:caption>I had the opportunity to execute aerodynamic surfacing for the inlets in Solidworks and Catia. The surfaces I generate were driven by curvature-controlled splines and lofted area-controlled profiles. The surfaces were then analyzed for performance and efficiency with CFD. Wind tunnel testing demonstrated that the outboard inlet achieved an efficiency of __% and there was extremely low variation between CPD predictions and Wind Tunnel Data (as shown in the image below).</image:caption>
    </image:image>
    <image:image>
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      <image:title>XB-1 Outboard Inlets</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614742409611-FTJMIDYSRGSGDWSWOPRI/ob+inlet+xb1+5x+deformation.gif</image:loc>
      <image:title>XB-1 Outboard Inlets</image:title>
      <image:caption>The under-wing inlets deflect outboard and upwards on the order of an inch. This deflection led to challenging sliding interfaces between the inlet and the fuselage and between the inlet and the wing.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614699455327-XELWU1ORJ45EYU6BYNK2/OB+inlet+5..PNG</image:loc>
      <image:title>XB-1 Outboard Inlets - Initial Structural Layout</image:title>
      <image:caption>Once we validated the loft surfaces, we laid out the composite primary structure and mechanism conceptual designs. The layout included frames that gave stiffness to the inlet duct and nacelle components, as well as actuated ramps and doors for optimizing engine efficiency across the flight envelope. The deflections between the inlets and the fuselage were high. As a result, determining constraints of the inlet attachment points was one of the most challenging aspects of the design.</image:caption>
    </image:image>
    <image:image>
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      <image:title>XB-1 Outboard Inlets</image:title>
      <image:caption>All components had minimum margins close to zero. This approach ensured that all our components were just stiff enough and just strong enough to withstand predicted flight loads. Most of our structure was sized by abrupt yaw cases and hammershock cases.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614699838654-K24B9X01T9JD3JLK8Q66/fs682+frame.PNG</image:loc>
      <image:title>XB-1 Outboard Inlets - Optimized Carbon-Composite Laminates</image:title>
      <image:caption>Once we had a conceptual design that closed, we proceeded to optimize all primary structure to reduce weight. Each colored region in the picture to the right indicates a different ply count. By reducing ply counts to only what was necessary for each region, we were able to reduce weight of frames by 22%.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614741586265-JT7VWK9B6MKM7XNF0XGZ/ob%2Binlet%2BCPD%2Bnacelle.jpg</image:loc>
      <image:title>XB-1 Outboard Inlets - Carbon-fiber Ply Design</image:title>
      <image:caption>I learned CPD from our leading composites expert at Boom. As a result, I was able to achieve within 2% of the predicted FEM stiffness in the as-built composite parts. The stiffness and quality of a composite part relies heavily on how the plies are spliced and darted and what seed points are chosen. Flattened patterns of nacelle plies are shown in the image to the left.</image:caption>
    </image:image>
    <image:image>
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      <image:title>XB-1 Outboard Inlets</image:title>
      <image:caption>View into the righthand inlet duct as the CFOAM tool is being chiseled away</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614741804478-5ZOKTPL5VCXJDCYLCTTT/IMG_3336.jpg</image:loc>
      <image:title>XB-1 Outboard Inlets - Assisted Fabrication at the Vendor</image:title>
      <image:caption>Due to weight savings optimization, the outboard inlet composite parts increased in complexity. Some composite frames (like the one shown below) had over 200 carbon fiber cut pieces that all needed to be placed with high accuracy. The inlet ducts were also extremely challenging to fabricate because the tool needed to be chiseled out by hand after the parts finished curing in the autoclave. As a result, it was vital to have engineering support on-site. While supporting in an engineering capacity, I also had the opportunity to layup parts I designed with experienced composite technicians.</image:caption>
    </image:image>
    <image:image>
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      <image:title>XB-1 Outboard Inlets</image:title>
      <image:caption>View of a tight corner in one of the outboard inlet frames. Tight corners required many darts and patch plies</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614743726294-WYM9L8WG5XDCC02ZGUBS/ob+inlet+layup.png</image:loc>
      <image:title>XB-1 Outboard Inlets</image:title>
      <image:caption>View of core being laid up on the lefthand inlet duct.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614744040623-SYRKNQV8NSO5BLZLRTES/ob+inlet+11.png</image:loc>
      <image:title>XB-1 Outboard Inlets - Supported Assembly and Nonconformances</image:title>
      <image:caption>The outboard inlets were jigged, bonded, and fastened in five weeks. This accelerated schedule required copious engineering support and diligent planning ahead. On the engineering side, I created work instructions, reviewed bond gaps with metrology, checked bond fillets, and create fastener vector files. However, I also got my hands dirty; I helped glue jigs to aircraft hardware, bond prep carbon fiber components, mix adhesive, fillet critical bonds, and pop a few rivets. This phase of the build has been my favorite aspect of the design cycle!</image:caption>
    </image:image>
    <image:image>
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      <image:title>XB-1 Outboard Inlets</image:title>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/j-85-engine-mice</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-17</lastmod>
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      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614804025246-XSZ7OV4OPC2NZZLUMMU0/IMG_0428.jpg</image:loc>
      <image:title>J-85 Engine Mice - Design Overview</image:title>
      <image:caption>Engine mice (shown in silver in the image to the left) attach to the inner nozzle flaps of an adjustable area nozzle. They are test parts that are used to constrict the area at the throat of the engine to get stall data across the engine operating environment. The engine mice were 3D printed out of Inconel, a nickel-based high temperature alloy. I designed these parts as my summer internship project at Boom.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614804525645-LJ7R6LY78T4LPONQ9160/engine+mice+engine+data.PNG</image:loc>
      <image:title>J-85 Engine Mice</image:title>
      <image:caption>NASA Compressor Map for similar engine test conditions</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614804382043-V1AJMSAMAIIZXCH9W3NR/engine+mice+npss.png</image:loc>
      <image:title>J-85 Engine Mice - Sizing</image:title>
      <image:caption>I created a solver in NPSS (a NASA engine performance software) to find choke area at the nozzle throat for different shaft speeds</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614804651876-GETIF1Z2HG685CBWT7TO/engine+mice+engine+data+better.PNG</image:loc>
      <image:title>J-85 Engine Mice</image:title>
      <image:caption>Stall and Nominal line from NPSS Solver Results described above. Compressor map shown on left was compared to plot above to verify solver results</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614805239727-CC1H0OAZUTF862GHWA4S/engine+mice+limit+stress.png</image:loc>
      <image:title>J-85 Engine Mice</image:title>
      <image:caption>Limit Stress Check</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614805260659-3W0V1TN2CJIJ38MC4V2K/engine+mice+buckling.png</image:loc>
      <image:title>J-85 Engine Mice</image:title>
      <image:caption>Buckling Check</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614804885427-GKA3C6UYGOFEIK1EGFBM/engine+mice+mock+up.jpg</image:loc>
      <image:title>J-85 Engine Mice - Design</image:title>
      <image:caption>I designed an aerodynamic, tight tolerance wedge that fastened to the nozzle flap. I generated a surface to interface with the nozzle flap by scanning the nozzle flap and creating a surface from the point cloud. I then analyzed the geometry in SolidWorks and 3D printed a mock-up to check fit.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614805276969-BA4QUZ6TVW37X768J47M/engine+mice+modal.png</image:loc>
      <image:title>J-85 Engine Mice</image:title>
      <image:caption>Modal Check</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614806160365-EXJ9PYLFMOI065G7M5HM/engine+mice+test+cell+2.png</image:loc>
      <image:title>J-85 Engine Mice</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614805969129-RM14QG6RMUM8VX0F3Z1D/engine+test+cell.jpg</image:loc>
      <image:title>J-85 Engine Mice - Testing</image:title>
      <image:caption>Engine mice achieved intended purpose at USAFA test cell. Data from engine operability testing informed engine face distortion requirements and XB-1 flight envelope. I had the opportunity to assist with testing by monitoring temperature limits in the control room (shown in the image below)</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/grain-boundary-research</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-17</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614866714011-B3MKISDY5WMNWYB2W4UT/grain+boundary+7.jpg</image:loc>
      <image:title>Grain Boundary Research - Research Overview</image:title>
      <image:caption>Research Objective: Create the first aluminum bicrystal with a planar grain boundary separating the two aluminum grains Bicrystal Method: (1) 3D print master, (2) cast plaster mold, (3) forge bicrystal with furnace, (4) machine bicrystal into required sample dimensions, (5) sample etching to remove surface imperfections Process Generation: Proprietary process developed by a PhD student, a material science student, and myself Research Purpose: Grain boundary control in materials is a growing field in additive manufacturing. Specifying grain boundaries can lead to superior shock absorption properties for missile defense and ISS/satellite external structure (Image on right shows samples made for the Army Research Labs. Samples were hypersonic shock tested.)</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614867656536-RCKMOS9TBGBKGOS64VCW/grain+boundary+4.PNG</image:loc>
      <image:title>Grain Boundary Research - From Theory to Execution</image:title>
      <image:caption>The proprietary process was developed by a PhD student, a material science student, and myself. It was the first time the theorized grain boundary control method (shown in the image to the left) had been executed in a lab. Developing the process required copious iteration and a high precision.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614868791363-DN7E3ZOYPJEB1R3R8OEO/IMG_0659.jpg</image:loc>
      <image:title>Grain Boundary Research - (1) 3D Print Master</image:title>
      <image:caption>Master is generated using Stereolithography (SLA) 3D printing. The crystal is highly sensitive to the dimensions of the master. A cusp too large between the two crystals or too small will cause the crystal to leave the metastable region and form multiple grains.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614868600584-L2CUVX7FOL3ZJCH3AXHB/molten-metal-in-crucible-5226099166.jpg</image:loc>
      <image:title>Grain Boundary Research - (2) Cast plaster mold</image:title>
      <image:caption>The 3D printed master is placed inside of the mold housing. Plaster is added then left to dry. Then, the mold is heated and the 3D printed master melts away. Finally, high purity aluminum is melted in a crucible and delicately poured into the mold.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614868634963-41Y7EGHNMP7OEVP9GFP7/grain+boundary+5.PNG</image:loc>
      <image:title>Grain Boundary Research - (3) Forge bicrystal with furnace</image:title>
      <image:caption>As the mechanical engineer on the team, I was tasked with designing the actuated furnace and machining methods. The furnace (labeled in the image to the right) starts low to the ground and moves upwards at a rate of 1 inch per hour to grow the two aluminum grains in a controlled and repeatable manner. A vacuum pump is also attached to the furnace to lower the pressure in the crystal growth chamber to reduce crystal impurities.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614913644465-RVL8TBJ8PWD5YS0TQ211/grain+boundary+3.png</image:loc>
      <image:title>Grain Boundary Research</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614913617240-BRKLXWQ5FGX1WF9NS87J/grain+boundary+2.png</image:loc>
      <image:title>Grain Boundary Research</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615652821179-EWENJX68B8AIPTYH24OR/grain%2Bboundary%2B6.jpg</image:loc>
      <image:title>Grain Boundary Research</image:title>
      <image:caption>After Machining</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615652785692-MDN7BLB83EBKOK2PFRHI/IMG_0661.jpg</image:loc>
      <image:title>Grain Boundary Research</image:title>
      <image:caption>Before Machining</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1614917277043-0LD2GN2XT88FFPXYGL4J/IMG_0294.jpg</image:loc>
      <image:title>Grain Boundary Research - (4) Machine bicrystal into required sample dimension</image:title>
      <image:caption>Machining a bicrystal is more challenging that stock aluminum billets because the metal is softer and requires slower feeds and faster speeds. I wrote the G-Code that cut the samples from the bicrystal.</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/highspeed-composter</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-17</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616020794734-2P1RN75ZUSQNCNN26IH7/compostmate%252B12.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616020536602-GQWPD26URAJTV2Y3UZB8/senior+design+3.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>Compost generated from food waste by the Compost-Mate in just 15 days (feat. complimentary 3D printed shovel)</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616016443253-659O3KSGQOPTEZQ56P9Q/Compostmate+10.2%60.PNG</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616014722154-Q6JSJE1VTTCFIDIMNRO2/compostmate+2.PNG</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>The Compost-Mate provides all functionality necessary to create compost while still being completely recyclable itself</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616021226201-YZGU5U2TOSBB4A3VAR7F/senior%2Bdesign%2B2.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616016609752-V4AXEG4F6XUU7Q9L3HE7/compostmate+8.png</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>We created a Functional Decomposition Chart to break down the complex nature of composting</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616016779605-D9RRS0OBQJB9E215YW9B/compostmate+11.PNG</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616023537520-028ZL9E9DPOE5IX9O31Y/compostmate%2B13.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616021064689-21ZY0IB9MXPBTHLHJV5W/Compostmate+5.png</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>HSB Living Lab Common Space - Final Resting Place of one of our Compost-Mate Prototypes</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616022749742-WPYHFEA8JBIAY9H9L6UL/compostmate+14.2.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616021077872-W5TR4O2TSUTSFOTWYT49/compostmate+4.png</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>HSB Living Lab, a Sustainable Apartment Complex in Sweden that trials innovative technologies</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616022346503-H6RWCZLOJQWKIIOF10ZN/compostmate%2B7.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1616022309167-HTY1P4RJIZ5XOJVRIKH8/compostmate%2B6.jpg</image:loc>
      <image:title>High-Speed Composter</image:title>
      <image:caption>HSB Living Lab Innovation Competition Finals</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/jet-engine-heat-shield</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-11</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615404980576-PMR3QZI6HOVF5LJGBKCG/hs%2Bthemral%2Bresults%2B1.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>No Heat Shield</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615404950329-8ZXIOQU9LO1IYGERQJ39/HS%2Bthermal%2Bresults%2B2.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>With Heat Shield</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615408383389-20EVPJOHQUBVPZ404JTB/heat%2Bshield%2Biteration.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615406707005-LFTXZ7PW33M0PQPEVUB9/heat%2Bshield%2Biteration.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615408481144-R9MX05DCO7G6JE49HCV1/hs%2Biteration%2B3%2Bthermal.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>The results above show the deflection of the heat shield at 1000 F. The deflection bands shown are a result of thermal growth alone.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615408707607-Z56HHLPBVZY13XGR1SFT/hs%2Biteration%2B3.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>We switched to frame attachments for both fwd and aft clips. We also split the heat shield into two discrete cantilevered sections. This change allowed the heat shield to grow freely. The skins remained just stiff enough to withstand sonic fatigue and the vibration environment</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615406431898-MII5WFID8G0UCBUE9ZVJ/heat%2Bshield%2Biteration.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615407400684-EEKMZJHA48Y87529DWBP/iteration+1+mode.png</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>The rigid fwd attachments picked up engine vibration that resulted in a 250g mode</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615408034395-AWWHO8OZ5KB1T5UFO1DY/hs%2Biteration%2B2.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>The aft attachments moved to a nearby aft fuselage frame. We thought that with the stiffer mounts attached to a frame, we would be able to handle engine vibration better. The heat shield became faceted for ease of manufacturability.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615407381445-H22SY93DILCE75KEMPBC/hs+iteration+0.png</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>The titanium heat shield was attached to the engine on the fwd and aft edges. The fwd attachments were rigid and the aft attachments were flexures to take up thermal growth</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615407952734-EB7MTK4EY77P20DMU9WC/image+%28153%29.png</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
      <image:caption>The fwd clips yielded due to lateral engine vibrations. If we made the clips stiffer, they would pick up more lateral engine vibration and fail sooner. If we made the clips thinner, the thermal stresses would cause the clips to fail sooner. Stalemate.</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615407905123-1LDYK07YVT1HN8RV4Z2W/heat%2Bshield%2Biteration.jpg</image:loc>
      <image:title>Jet Engine Heat Shield</image:title>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/eclipse-rocket-injector-plate</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-17</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615902231386-LLELRCJJPNXQH328FDCP/injector%2Bplate%2B4.jpg</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Injector plate bulkhead analysis</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615902424092-8MTW4YPSL28LZ7XFQX5J/eclipse+nozzle+test+fixture.jpg</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Test Stand Assembly Drawing</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615901809459-EQLYFNKQOMH4FEST2OMD/injector+plate+6.png</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Test Injector Plate with Injector Nozzles</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615902189589-HX42ZT2TCH7CYQG42327/injector+plate+full+assy+analysis.png</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Primary Structure Analysis</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615902440581-FYCODUYT5VKIXQJCWGTR/eclipse+ignition+test.jpg</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Flight-Scale Hybrid Rocket Engine Ignition Testing, 2018</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615653648680-KTGJ1INZML7Y3QHQYOBQ/injector+plate+9.png</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Hybrid Rocket Engine, Initial Design</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615902389576-F5MRL12VUMIR17HVFMIM/eclipse+injector+plate+bulkhead.png</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Injector Plate Bulkhead Drawing</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615653666194-K15X2MBUEXJUQ5HY8L3M/injector+plate+10.jfif</image:loc>
      <image:title>Eclipse Rocket Injector Plate</image:title>
      <image:caption>Hybrid Rocket Engine Test Stand</image:caption>
    </image:image>
  </url>
  <url>
    <loc>https://carolinekrawczyk.com/water-desalination-startup</loc>
    <changefreq>daily</changefreq>
    <priority>0.75</priority>
    <lastmod>2021-03-17</lastmod>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615906585507-3B0VLR30BAQXQJQTQ3LO/mis+8.jpg</image:loc>
      <image:title>Water Desalination Startup</image:title>
      <image:caption>Cutting the fiberglass housing of the test small-scale test cell</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615906513765-ZTFV7KHKIWYIEJYG9GIO/mis+9.jpg</image:loc>
      <image:title>Water Desalination Startup</image:title>
      <image:caption>Filtration Performance Test Bench</image:caption>
    </image:image>
    <image:image>
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      <image:title>Water Desalination Startup</image:title>
      <image:caption>Then: 2016 Desalination Cell - Proof of Concept</image:caption>
    </image:image>
    <image:image>
      <image:loc>https://images.squarespace-cdn.com/content/v1/6012c667333305652fe566f8/1615906422065-HJO3VTJYB5TYBPKVZSLO/MIS+1.jpg</image:loc>
      <image:title>Water Desalination Startup</image:title>
      <image:caption>Material deposition on the cathode after electrode connection joint testing</image:caption>
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    <image:image>
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      <image:title>Water Desalination Startup</image:title>
      <image:caption>Now: 2020 Full Scale Desalination Unit - Currently Operating</image:caption>
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    <image:image>
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      <image:title>Water Desalination Startup</image:title>
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    <image:image>
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      <image:title>Water Desalination Startup</image:title>
      <image:caption>One of the first, scrappy proof-of-concept tests aimed at replicating the CEO’s results</image:caption>
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