Investigation of unsteady subsonic spoiler and flap aerodynamics-Reference-Cited by-同舟云学术

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Investigation of unsteady subsonic spoiler and flap aerodynamics

Published:1987-09 Issue:9 Volume:24 Page:629-637
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Costes M.¹,Gravelle A.¹,Philippe J.¹,Vogel S.²,Triebstein H.³

Affiliation:

1. Office National d'Etudes et de Recherches Aerospatiales, Chatillon, France

2. Messerschmidt-Bolkow-Blohm Gmbtt, Bremen, Federal Republic of Germany

3. Deutsche Forschungs-und Versuchsanstalt fur Luft-und Raumfahrt e. V., Gottingen, Federal Republic of Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45488

Reference4 articles.

1. Calculation method for transonic separated flows over airfoils including spoiler effects

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