Variation of Transition Reynolds Number with Mach Number-Reference-Cited by-同舟云学术

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Variation of Transition Reynolds Number with Mach Number

Published:1953-10 Issue:10 Volume:20 Page:718-719
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

Lange A. H.¹,Gieseler L. P.¹,Lee R. E.¹

Affiliation:

1. U.S. Naval Ordnance Laboratory, White Oak, Silver Spring, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2804

Reference9 articles.

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. Boundary-layer transition on a slender cone in hypersonic flow;AIAA Journal;1964-04

2. Some Features of Boundary Layers and Transition to Turbulent Flow;Journal of the Aeronautical Sciences;1956-05

3. Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8;Journal of the Aeronautical Sciences;1956-02

4. Transonic Flow Past Wedge Profiles by Hydraulic Analogy;Journal of the Aeronautical Sciences;1954-07

5. Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels;Journal of the Aeronautical Sciences;1954-07

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