Transition Research in Low-Disturbance High-Speed Wind Tunnels-Reference-Cited by-同舟云学术

Transition Research in Low-Disturbance High-Speed Wind Tunnels

Published:1990 Issue: Volume: Page:227-238
ISSN:
Container-title:Laminar-Turbulent Transition
language:
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Author:

Beckwith I. E.,Chen F.-J.,Malik M. R.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-84103-3_19.pdf

Reference29 articles.

1. Pate, S. R.; and Schueler, C. J.: Radiated Aerodynamic Noise Effects on Boundary-Layer Transition in Supersonic and Hypersonic Wind Tunnels. AIAA J. 7(3) (1969) 450–457. Also, AEDC-TR-67–236 (1968).

2. Pate, S. R: Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds. AIAA J. 9(6) (1971) 1082–1090. Also, AEDC-TR-69–172 (1969).

3. Pate, S. R: Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic-Hypersonic Wind Tunnels - Theory and Application. Arnold Engineering Development Center, Arnold Air Force Station, TN, AEDC-TR-77–107 (1978).

4. Stainback, P. C.: Hypersonic Boundary Layer Transition in the Presence of Wind-Tunnel Noise. AIAA J. 9 (12) (1971) 2475–2476.

5. Stainback, P. C.: Part I: Measurement of Transition Reynolds Numbers and Surface Pressure. Fischer, M. C.; and Wagner, R. D.: Part II: Transition and Hot-Wire Measurements up to a Local Mach Number of 16 in Helium. Effects of Wind Tunnel Disturbances on Hypersonic Boundary Layer Transition. AIAA Paper No. 72–181, January 1972.

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