Three-Dimensional Flow Separations on Aircraft and Missiles
- 1 May 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (5), 567-580
- https://doi.org/10.2514/3.50159
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Investigation of the leeward side of a delta wing at hypersonic speeds.Journal of Spacecraft and Rockets, 1969
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- Analysis and design of wing-body combinations at subsonic and supersonic speeds.Journal of Aircraft, 1968
- Wake survey of powered and unpowered C-5A aircraft modelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Turbulent boundary-layer separation ahead of cylinders.AIAA Journal, 1968
- Aerodynamic Design Features of the C‐5AAircraft Engineering and Aerospace Technology, 1968
- Calculation of pressure distributions on cambered bodies of arbitrary cross section at angle of attack with application to transport fuselage afterbody designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Some aerodynamic principles for the design of swept wingsProgress in Aerospace Sciences, 1962
- The Determination of Turbulent Skin Friction by Means of Pitot TubesJournal of the Royal Aeronautical Society, 1954