Calculation of unsteady airfoil loads with and without flap deflection at -90 degrees incidence-Reference-Cited by-同舟云学术

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Calculation of unsteady airfoil loads with and without flap deflection at -90 degrees incidence

Published:1991-08-17 Issue: Volume: Page:
ISSN:
Container-title:9th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

STREMEL PAUL¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-3336

Reference11 articles.

1. 3Cordova,J.Q.andBarth,T.J. "GridGenerationfor General2-DRegionsUsing HyperbolicEquations," AIAAPaper 88-0520,1988.

2. 4Maisel,M. D., Laub,G. H., andMcCroskey,W.J. "AerodynamicCharacteristicsofTwo-DimensionalWing ConfigurationsatAnglesof AttackNear-90Degrees," NASATM-88373,1986.

3. SFelker,F.F.,Shinoda,P.R.,Heffernan,R.M., and Sheehy,H. F."WingForceandSurfacePressureData from aHoverTestof a0.658-Scale V-22Rotorand Wing,"NASATM-102244,1990.

Cited by 2 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. Effect of fences on airfoil aerodynamics at -90 degree incidence;AIAA Journal;1996-10

2. Effect of Reynolds number and turbulence on airfoil aerodynamics at -90-degree incidence;AIAA Journal;1994-03

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