Calculated Transonic Flow Past Slender Fuselages and Afterbodies
- 1 September 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (9) , 710-716
- https://doi.org/10.2514/3.59161
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- On the Prediction of Mixed Subsonic/Supersonic Pressure DistributionsJournal of the Aerospace Sciences, 1960
- A Refinement of the Linearized Transonic Flow TheoryJournal of the Physics Society Japan, 1960