Critical layer concept relative to hypersonic boundary layer stability-Reference-Cited by-同舟云学术

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Critical layer concept relative to hypersonic boundary layer stability

Published:1985-01-14 Issue: Volume: Page:
ISSN:
Container-title:23rd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

NAGAMATSU H.¹,SHEER, JR. R.²

Affiliation:

1. Rensselaer Polytechnic Institute, Troy, NY

2. GE Research and Development Center, Schenectady, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-303

Reference33 articles.

1. Lees, L. "The Stabilitv of the Laminar Bound ary Layer ina Compressible Fluid," NACA, TR 876 ,1947.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K;Journal of Propulsion and Power;1993-01

2. Investigation of the stability characteristics of a compressible boundary layer on a flat plate at high mach number;Journal of Applied Mechanics and Technical Physics;1992

3. Investigation of a 2-D Scramjet inlet, freestream M = 8.25 and T sub0 = 800-4,100 K;3rd International Aerospace Planes Conference;1991-08-17

4. Experimental investigation of a 2-D scramjet inlet at Mach numbers of 8 to 18 and stagnation temperatures of 4,100K;29th Aerospace Sciences Meeting;1991-01-07

5. Wall cooling effects on hypersonic boundary layer transition, M(1) =7.5 - 15;4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference;1986-05-12

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