Theoretical analysis of aircraft afterbody flow
- 25 June 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A computational investigation of supersonic axisymmetric flow over boattails containing a centered propulsive jetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Numerical Simulation of Three-Dimensional Boattail Afterbody FlowfieldsAIAA Journal, 1981
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- Optimization of Drag Minimums Including Effects of Flow SeparationJournal of Engineering for Industry, 1973
- Thrust-minus-drag optimization by base bleed and/or boattailingJournal of Spacecraft and Rockets, 1970