Effect of Simulated Jet Engines on the Flowfield behind a Swept-Back Wing
- 1 April 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (4), 343-349
- https://doi.org/10.2514/3.58783
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Flow survey behind wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Wind Tunnel Measurements of Rolling Moment in a Swept-Wing Vortex WakeJournal of Aircraft, 1976
- Wind-Tunnel Studies of Wing Wake TurbulenceJournal of Aircraft, 1972
- Measurements of Boeing 747, Lockheed C5A and Other Aircraft Vortex Wake Characteristics by Tower Fly-by TechniquePublished by Springer Nature ,1971