Peter Sturdza, Ph.D.
Affiliations: | 2004 | Stanford University, Palo Alto, CA |
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Aerospace EngineeringGoogle:
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Publications
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Sturdza P, Rajnarayan D. (2014) Design and validation of a supersonic natural laminar flow test article Aiaa Aviation 2014 -15th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference |
Rajnarayan D, Sturdza P. (2013) Extensible rapid transition prediction for aircraft conceptual design using modal decomposition 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013 |
Sturdza P, Suzuki Y, Martins-Rivas H, et al. (2012) A quasi-simultaneous interactive boundary-layer model for a cartesian euler solver 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
Rajnarayan D, Sturdza P. (2011) Extensible rapid transition prediction for aircraft conceptual design 29th Aiaa Applied Aerodynamics Conference 2011 |
Allison E, Kroo I, Sturdza P, et al. (2010) Aircraft conceptual design with natural laminar flow 27th Congress of the International Council of the Aeronautical Sciences 2010, Icas 2010. 1: 428-436 |
Sturdza P. (2007) Extensive supersonic natural laminar flow on the aerion business jet Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 12: 8465-8481 |
Rodriguez DL, Sturdza P. (2006) A rapid geometry engine for preliminary aircraft design Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 15: 11104-11115 |
Wintzer M, Sturdza P, Kroo I. (2006) Conceptual design of conventional and oblique wing configurations for small supersonic aircraft Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 15: 11116-11132 |
Kroo I, Sturdza P. (2003) Design- oriented aerodynamic analysis for supersonic laminar flow wings 41st Aerospace Sciences Meeting and Exhibit |
Kroo I, Tracy R, Chase J, et al. (2002) Natural laminar flow for quiet and efficient supersonic aircraft 40th Aiaa Aerospace Sciences Meeting and Exhibit |