Application of nonlinear indicial modeling to the prediction of a dynamically stalling wing-Reference-Cited by-同舟云学术

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Application of nonlinear indicial modeling to the prediction of a dynamically stalling wing

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:14th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Reisenthel Patrick¹

Affiliation:

1. Nielsen Engineering and Research, Inc., Mountain View, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2493

Cited by 8 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. Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow;Chinese Journal of Aeronautics;2018-04

2. Nonlinear Unsteady Aerodynamic Modeling Using Wind-Tunnel and Computational Data;Journal of Aircraft;2017-03

3. On the generation of flight dynamics aerodynamic tables by computational fluid dynamics;Progress in Aerospace Sciences;2011-11

4. Use of Piloted Simulation for Evaluation of Abrupt-Wing-Stall Characteristics;Journal of Aircraft;2005-05

5. A Review of Unsteady Aerodynamic Modelling for Flight Dynamics of Manoeuvrable Aircraft;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2004-06-22

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