Development and Application of a New Unsteady Far-Field Drag Decomposition Method-Reference-Cited by-同舟云学术

Development and Application of a New Unsteady Far-Field Drag Decomposition Method

Published:2015-11 Issue:11 Volume:53 Page:3414-3429
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Toubin Hélène¹,Bailly Didier¹

Affiliation:

1. Applied Aerodynamics Department, ONERA–The French Aerospace Lab, F92190 Meudon, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054002

Reference37 articles.

1. VKI Lecture Series;Van Dam C.-P.,2003

2. BetzA. “A Method for the Direct Determination of Wing-Section Drag,” Zeitschrift für Flugtechnik und Motorluftschiffahrt, NACA TM-337, Feb. 1925, pp. 42–44 (in German).

3. OswatitschK., Gas Dynamics, Academic Press, New York, 1956, pp. 207–210.

4. MaskellE.C. “Progress Towards a Method for the Measurement of the Components of Drag for a Wing of Finite Span,” Royal Aircraft Establishment TR-72232, 1972.

5. Shock Waves and Drag in the Numerical Calculation of Compressible, Irrotational Transonic Flow

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