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Air Breathing Engine Testing in the Propulsion Wind Tunnel Facility of the Arnold Engineering Development Center

Published online by Cambridge University Press:  04 July 2016

R. W. Hensel  and
M. Pindzola
R. W. Hensel
Affiliation:
ARO, Inc
M. Pindzola
Affiliation:
ARO, Inc
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Extract

The purpose of this paper is to further illustrate the utility of a wind tunnel (see refs. 1 and 2) in providing performance date on aircraft engine installations. The discussion is limited to the test work accomplished in the Propulsion, Wind Tunnel Facility (PWT) at the Arnold Engineering Development Center (AEDC) at Tullahoma, Tennessee, USA

Type
Symposium on Altitude Testing
Information
The Aeronautical Journal , Volume 74 , Issue 711 , March 1970 , pp. 197 - 205
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

1. Hensel, R. W. and Matt, H. K. Full-scale Propulsion Testing in Wind Tunnels. AGARDograph 37, pp. 79–128, 1961.Google Scholar
2. Pindzola, M. and Delano, J. B. Wind Tunnel Testing of Propulsion Systems. AIAA Paper No. 65–477, 1965.Google Scholar
3. Bellman, D. R. and Hughes, D. L. The Flight Investigation of Pressure Phenomena in the Air Intake of an F-111A Airplane. AIAA Paper No. 69–488, 1969.Google Scholar
4. Coltrin, R. E. and Calogeras, J. E. Supersonic Wind Tunnel Investigation of Inlet-Engine Compatibility. AIAA Paper No. 69–487, 1969.Google Scholar