Oscillating Airfoils: Part 11. Newtonian Flow Theory and Application to Power-Law Bodies in Hypersonic Flow-Reference-Cited by-同舟云学术

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Oscillating Airfoils: Part 11. Newtonian Flow Theory and Application to Power-Law Bodies in Hypersonic Flow

Published:1978-11 Issue:11 Volume:16 Page:1132-1138
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Barren Ronald M.¹,Mandl P.²

Affiliation:

1. University of Windsor, Windsor, Ontario, Canada

2. Carleton University, Ottawa, Ontario, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61019

Reference10 articles.

1. ^clntosh, Jr., S. C. "Studies in Unsteady Hypersonic Flow Theory," Ph.D. Dissertation,Stanford University, Aug. 1965.

2. Barren, R. M. "Unsteady Newtonian Flow Past Oscillating Bodies with Application to Airfoils Supporting Power-Law Shocks," Ph.D. Dissertation,Carleton University, June 1974.

Cited by 6 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

2. Newtonian and hypersonic flows over oscillating bodies of revolution—I. Circular cones;Acta Astronautica;1993-04

3. Oscillating two-dimensional hypersonic airfoils at small angles of attack;AIAA Journal;1992-03

4. Newtonian flow over oscillating two-dimensional airfoils at moderateor large incidence;AIAA Journal;1990-04

5. Unsteady supersonic flow past a harmonically pitching and plunging cone;7th Atmospheric Flight Mechanics Conference;1981-08-17

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