| Document Date: 2014-06-16 01:13:10
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City Honolulu / Palo Alto / / Company NASA Langley / Desktop Aeronautics Inc. / the Boeing / Astronautics Inc. / / Facility American Institute of Aeronautics / / IndustryTerm engine technologies / transition prediction tool / fidelity aerodynamics solutions / technology impact / aerospace industry / stand-alone tool / non-similar solution / Similarity solutions / suitable design tools / self-similar solutions / air travel / natural laminar-flow technology / manufacturing tolerances / database processing scheme / oil prices / active laminar flow control applications / clean boundary-layer solutions / case neural networks / database-building tools / laminar fluctuation kinetic energy / transition-prediction tools / / Organization American Institute of Aeronautics / National Aeronautics and Space Administration / AIAA / / Person Dev Rajnarayan / Warren / Hassan / Peter Sturdza / Drela / / Position President of Research and Development / representative / Engineer /Scientist / / Product LASTRAC11 software / F-14 / swept wing / F-111 NLF / Falcon / A320 / LASTRAC11 / / ProgrammingLanguage K / / ProvinceOrState California / / Technology natural laminar-flow technology / flow control / engine technologies / /
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29th AIAA Applied Aerodynamics Conference, June 27–30, Honolulu, Hawaii Extensible Rapid Transition Prediction for Aircraft Conceptual Design Dev Rajnarayan∗