Calculations of the flow past bluff bodies, including tilt-rotor wing sections at alpha = 90 deg
Author:
Affiliation:
1. Sterling Software, Palo Alto, CA
2. NASA, Ames Research Center; U.S. Army, AeroflightdynamicsDirectorate, Moffett Field, CA
3. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-32
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Simulation and analysis of V-22 tiltrotor aircraft forward-flight flowfield;Journal of Aircraft;1996-03
2. Simulation and analysis of V-22 tiltrotor aircraft forward flight flowfield;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
3. Simulation of V-22 rotorcraft hover flowfield;International Powered Lift Conference;1993-08-22
4. Navier-Stokes computation of wing/rotor interaction for a tilt rotor in hover;AIAA Journal;1992-11
5. Calculation of flow about two-dimensional bodies by means of the velocity-vorticity formulation on a staggered grid;29th Aerospace Sciences Meeting;1991-01-07
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