Effect of Unsteady Pressure Gradient Reduction on Dynamic Stall Delay-Reference-Cited by-同舟云学术

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Effect of Unsteady Pressure Gradient Reduction on Dynamic Stall Delay

Published:1971-10 Issue:10 Volume:8 Page:839-841
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

CARTA FRANKLIN O.¹

Affiliation:

1. United Aircraft Research Laboratories, East Hartford, Conn.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.59179

Reference9 articles.

1. Halfman, R. L., Johnson, H. C., and Haley, S. M. "Evaluation of High-Angle-of-Attack Aerodynamic-Derivative Data and Stall-Flutter Prediction Techniques," TN 2533, Nov.1951, NACA.

2. Fung, Y. C., An Introduction to the Theory of Aeroelasticity, Wiley, New York, 1955, pp.452-453.

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