Propulsion/airframe integration and optimization on a supersonic business jet

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 18, Issue , 2007, Pages 12620-12630

  Rodriguez, David L ^a,b  

^a Desktop Aeronautics Inc   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; CIVIL AVIATION; COMPUTATIONAL FLUID DYNAMICS; CONSTRAINT THEORY; EULER EQUATIONS; NOZZLES; OPTIMIZATION; SUPERSONIC AERODYNAMICS;

AERODYNAMIC EFFICIENCY; AIRCRAFT AERODYNAMIC EFFICIENCY; NOZZLE INSTALLATIONS; SUPERSONIC BUSINESS JETS;

JETS;

EID: 34250843118     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1048     Document Type: Conference Paper

References (8)

1. Rodriguez, D.L., "Response Surface Based Optimization with a Cartesian CFD Method," AIAA-2003-0465, January 2003.
2. Rodriguez, D.L., "Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method," AIAA-2004-4492, August 2004.
3. Sanders, B.W., Koncsek, J.L., Hedges, L.S., The Boeing Company, Seattle, WA, U. S. Patent for a "Supersonic External-Compression Diffuser and Method for Designing Same," Patent No. 6,793,175 B1, Issued on September 21, 2004.
4. Rodriguez, D.L. and Sturdza, P., "A Rapid Geometry Engine for Preliminary Aircraft Design," AIAA-2006-0929, January 2006.
5. Aftosmis, M.J., Berger, M. J., and Adomavicius, G., "A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries", AIAA-2000-0808, January 2000.
6. Nash, J., Compact Numerical Methods for Computers: Linear Algebra and Function Minimisation, 2nd Ed., Adam Hilger Ltd. (Institute of Physics Publishing), September 1990, pp. 141-144.
7. Garzon, G.A., "Use of a Translating Cowl on a SSBJ for Improved Takeoff Performance," AIAA-2007-0830, January 2007.
8. Rodriguez, D.L., "A Multidisciplinary Optimization Method for Designing Boundary Layer Ingesting Inlets," AIAA-2002-5665, September 2002.