SOME FACTORS AFFECTING THE DYNAMIC STABILITY DERIVATIVES OF A FIGHTER-TYPE MODEL.

W. Staudacher; P. Poisson-Quinton; M. Canu; B. Laschka; B. Schulze

SOME FACTORS AFFECTING THE DYNAMIC STABILITY DERIVATIVES OF A FIGHTER-TYPE MODEL.

W. Staudacher, P. Poisson-Quinton, M. Canu, B. Laschka, B. Schulze

Chair of Aerodynamics and Fluid mechanics

Research output: Contribution to journal › Conference article › peer-review

Abstract

Dynamic stability coefficients of a fighter-type pilot model have been experimentally derived. In the first test phase, forced oscillation tests were carried out with this model in the ONERA wind tunnel. The angle of attack regime investigated was alpha equals 0 plus 25 degree . This first test phase was concentrated on the investigation of the effects of a strake on the total derivatives of the configuration.

Original language	English
Pages (from-to)	11. 1-11. 13
Journal	AGARD Conference Proceedings
Issue number	235
State	Published - 1978
Event	Dyn Stab Parameters, Pap and Discuss Presented at the Fluid Dyn Panel Symp - Athens, Greece Duration: 22 May 1978 → 24 May 1978

Cite this

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title = "SOME FACTORS AFFECTING THE DYNAMIC STABILITY DERIVATIVES OF A FIGHTER-TYPE MODEL.",

abstract = "Dynamic stability coefficients of a fighter-type pilot model have been experimentally derived. In the first test phase, forced oscillation tests were carried out with this model in the ONERA wind tunnel. The angle of attack regime investigated was alpha equals 0 plus 25 degree . This first test phase was concentrated on the investigation of the effects of a strake on the total derivatives of the configuration.",

author = "W. Staudacher and P. Poisson-Quinton and M. Canu and B. Laschka and B. Schulze",

year = "1978",

language = "English",

pages = "11. 1--11. 13",

journal = "AGARD Conference Proceedings",

issn = "0549-7191",

number = "235",

note = "Dyn Stab Parameters, Pap and Discuss Presented at the Fluid Dyn Panel Symp ; Conference date: 22-05-1978 Through 24-05-1978",

}

TY - JOUR

T1 - SOME FACTORS AFFECTING THE DYNAMIC STABILITY DERIVATIVES OF A FIGHTER-TYPE MODEL.

AU - Staudacher, W.

AU - Poisson-Quinton, P.

AU - Canu, M.

AU - Laschka, B.

AU - Schulze, B.

PY - 1978

Y1 - 1978

N2 - Dynamic stability coefficients of a fighter-type pilot model have been experimentally derived. In the first test phase, forced oscillation tests were carried out with this model in the ONERA wind tunnel. The angle of attack regime investigated was alpha equals 0 plus 25 degree . This first test phase was concentrated on the investigation of the effects of a strake on the total derivatives of the configuration.

AB - Dynamic stability coefficients of a fighter-type pilot model have been experimentally derived. In the first test phase, forced oscillation tests were carried out with this model in the ONERA wind tunnel. The angle of attack regime investigated was alpha equals 0 plus 25 degree . This first test phase was concentrated on the investigation of the effects of a strake on the total derivatives of the configuration.

UR - https://www.scopus.com/pages/publications/0018282972

M3 - Conference article

AN - SCOPUS:0018282972

SN - 0549-7191

SP - 11. 1-11. 13

JO - AGARD Conference Proceedings

JF - AGARD Conference Proceedings

IS - 235

T2 - Dyn Stab Parameters, Pap and Discuss Presented at the Fluid Dyn Panel Symp

Y2 - 22 May 1978 through 24 May 1978

ER -

SOME FACTORS AFFECTING THE DYNAMIC STABILITY DERIVATIVES OF A FIGHTER-TYPE MODEL.

Abstract

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