The Boundary Layer on a Sharp Cone in High-Enthalpy Flow-Reference-Cited by-同舟云学术

The Boundary Layer on a Sharp Cone in High-Enthalpy Flow

Published:1995 Issue: Volume: Page:63-68
ISSN:
Container-title:Shock Waves @ Marseille I
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Author:

Germain P.,Hornung H.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-78829-1_9.pdf

Reference9 articles.

1. Demetriades A (1974) Hypersonic viscous flow over a slender cone, Part III: Laminar instability and transition. AIAA Paper 74–535. Palo Alto, California

2. Di Cristina V (1970) Three-dimensional laminar boundary-layer transition on a sharp 8° cone at Mach 10. AIAA J. 8, 5: 852–856

3. Germain P, Cummings E, Hornung H (1993) Transition on a sharp cone at high enthalpy; new measurements in the shock tunnel T5 at GALCIT. AIAA Paper 93–0343, Reno, Nevada

4. Kendall JM (1975) Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition. AIAA J. 13, 3: 290–299

5. King RA (1992) Three-dimensional boundary-layer transition on a cone at Mach 3.5. Experiments in Fluids 13: 305–314

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