Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch-Reference-Cited by-同舟云学术

Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch

Published:1984-08 Issue:8 Volume:21 Page:576-582
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ricketts Rodney H.¹,Sandford Maynard C.¹,Seidel David A.¹,Watson Judith J.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45026

Reference8 articles.

1. Hess R. W. Wynne, E C , and Cazier F W Jr Static and Unsteady Pressure Measurements on a 50 Degree Clipped Delta Wing at M= 0 9 " AIAA Paper 820686 (also available as NASA TM 83297 April 1982)

2. 2Sandford M C Ricketts, R H , Cazier F W Jr , and Cun ningham H J Transonic Unsteady Airloads on an Energy Ef ficient Transport Wing with Oscillating Control Surfaces Journal of Aircraft Vol18,July 1981pp557561

3. 6Tijdeman, H , Investigations of the Transonic Flow Around Oscillating Airfoils, ' National Aerospace Laboratory, Amsterdam NLRTR 77090 U 1977 (available from DTIC as AD B027 633)

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