Aerodynamic control surface/trim tab coupling coefficients in subsonic two-dimensional unsteady flow /Coefficients aerodynamiques de couplage gouverne-tab, en ecoulement subsonique bidimensionnel instationnaire

Author: Dat, R
Published: [Place of publication not identified] : [publisher not identified], 1969.
Physical Description: pages 60-63
Additional Creators: American Institute of Aeronautics and Astronautics. Technical Information Service

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Language Note

In French.

Subject(s)

Collection

IAA papers.

Note

A69-33597.
Abstracted in International Aerospace Abstracts.
Reproduced from: La Recherche Aerospatiale

Reproduction Note

Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]

View MARC record | catkey: 19137855

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