Nonadiabatic Surface Effects on Transition Measurements Using Temperature-Sensitive Paints-Reference-Cited by-同舟云学术

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Nonadiabatic Surface Effects on Transition Measurements Using Temperature-Sensitive Paints

Published:2015-05 Issue:5 Volume:53 Page:1172-1187
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Costantini Marco¹,Fey Uwe¹,Henne Ulrich¹,Klein Christian¹

Affiliation:

1. Institute of Aerodynamics and Flow Technology, DLR, German Aerospace Research Center, D-37073 Göttingen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053155

Reference54 articles.

1. LeesL. “The Stability of the Laminar Boundary Layer in Compressible Fluid,” NACA Rept. 876, 1947.

2. Laminar-turbulent transition prediction in three-dimensional flows

3. Boundary-Layer Theory

4. LeesL.LinC. C. “Investigation of the Stability of the Laminar Boundary Layer in a Compressible Fluid,” NACA TN-1115, 1946.

5. ReshotkoE. “Control of Boundary-Layer Transition,” AIAA Paper 1985-0562, March 1985.

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