Nacelle aerodynamic design and integration study on a Mach 2.2 supersonic cruise aircraft
- 26 July 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Unique applications of the method of characteristics to inlet and nozzle design problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A computer method for dynamic structural analysis using stiffness matrices.Journal of Aircraft, 1969