Comment on 'Measurements in the laminar near-wake of magnetically suspended cones at freestream Mach number of 6.3'-Reference-Cited by-同舟云学术

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Comment on 'Measurements in the laminar near-wake of magnetically suspended cones at freestream Mach number of 6.3'

Published:1977-06 Issue:6 Volume:15 Page:891-892
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Crane R.I.¹

Affiliation:

1. Imperial College of Science & Technology, London, U.K.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.7385

Reference13 articles.

1. Measurements in the laminar near-wake of magnetically suspended cones at freestream Mach number = 6.3

2. 2Wilson, A. and Luff, B, "The Development, Design and Construction of a Magnetic Suspension System for the R. A.E. 7 in. x 7 in. Hypersonic Wind Tunnel," Royal Aircraft Establishment, Farnborough, Technical Report 66248,1966.

3. 3Crane, J.F.W. "Performance Aspects of the R.A.E. Magnetic Suspension System for Wind Tunnel Models", Royal Aircraft Establishment, Farnborough, Technical Report 68274,1968.

4. A Survey of Hypersonic Near Wake Studies

Cited by 2 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. Numerical computation of hypersonic laminar near-wake flow via Navier-Stokes solver;18th Fluid Dynamics and Plasmadynamics and Lasers Conference;1985-07-16

2. Computational probing of hypersonic laminar wakes;17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1984-06-25

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