Determination of stability and control derivatives using computational fluid dynamics and automatic differentiation-Reference-Cited by-同舟云学术

Determination of stability and control derivatives using computational fluid dynamics and automatic differentiation

Published:1999-06-28 Issue: Volume: Page:
ISSN:
Container-title:17th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Park Michael¹,Green Lawrence²,Montgomery Raymond²,Raney David²

Affiliation:

1. George Washington Univ., Washington, DC

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3136

Reference40 articles.

1. inley, D. "Euler TechnologyAssessmentProgram for PreliminaryAircraft DesignEmployingSPLITFLOW CodeWith CartesianUnstructuredGridMethod,"NASA CR-4649,Mar. 1995.

2. 2Charlton, E. "Numerical Stability and Control AnalysisTowardsFalling-LeafPredictionCapabilitiesof Splitflow for two Generic High-PerformanceAircraft Models,"NASA CR-1998-208730,Sept.1998.

3. 4Carle,A., Green,L., Bischof, C., andNewman,P. "Applications of Automatic Differentiation in CFD," AIAA Paper94-2197,June1994.

4. arle, A., Fagan,M., and Green,L. "Preliminary Results From the Application of Automated Adjiont CodeGenerationtoCFL3D"AIAA Paper98-4807,Sept. 1998.

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