A Rigidly Forced Oscillation System for Meaasuring Dynamic-stability Parameters in Transonic and Supersonic Wind Tunnels PDF Download
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Author: Albert L. Braslow
Publisher:
ISBN:
Category : Guidance systems (Flight)
Languages : en
Pages : 48
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Book Description
Author: Albert L. Braslow
Publisher:
ISBN:
Category : Guidance systems (Flight)
Languages : en
Pages : 48
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Book Description
Author: Albert L. Braslow
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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Book Description
PERIMENTAL DATA, Mathematical analysis, Errors.) The mechanical and electrical details of a sting-mounted, rigidly forced, single-degree-offreedom, oscillating yaw mechanism is described. The equipment was designed for use in transonic and supersonic wind tunnels. Dynamic-stability parameters measured with the equipment are uninfluenced by airstream turbulence or buffeting. Aerodynamically unstable bodies do not cause the mechanism to diverge, and configurations with negative damping can be tested. The accuracy of the system was investigated by application of known eddy-current damping moments. Typical wind-tunnel results are presented for the damping in yaw and oscillatory directional stability of a simplified airplane model with 45 degrees sweptback wing and vertical tail at transonic speeds. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
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Book Description
Author: Bruce R. Wright
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
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Book Description
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 990
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 252
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Book Description
Author: AIAA Aerodynamic Testing Conference
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 258
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Book Description
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 522
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
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