Summary of Theoretical, Experimental, & Computational Investigation of Flow Over Flat Plate to Mach 25-Reference-Cited by-同舟云学术

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Summary of Theoretical, Experimental, & Computational Investigation of Flow Over Flat Plate to Mach 25

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Nagamastu Henry¹,Myrabo Leik¹,Messitt D.²,Sheer R.³

Affiliation:

1. Rensselaer Polytechnic Institute

2. Aerojet Corp.

3. General Electric Global Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-506

Reference30 articles.

1. An Experimental Investigation of Leading-Edge Shock-Wave - Boundary-Layer Interaction at Mach 5.8

2. Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic Speeds

3. On the Use of the Neutral Point as a Stability Parameter

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