Author: Albert L. Braslow
Publisher:
ISBN:
Category : Guidance systems (Flight)
Languages : en
Pages : 48
Book Description
A Rigidly Forced Oscillation System for Meaasuring Dynamic-stability Parameters in Transonic and Supersonic Wind Tunnels
Author: Albert L. Braslow
Publisher:
ISBN:
Category : Guidance systems (Flight)
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Guidance systems (Flight)
Languages : en
Pages : 48
Book Description
A Rigidly Forced Oscillation System for Measuring Dynamic-stability Parameters in Transonic and Supersonic Wind Tunnels
Author: Albert L. Braslow
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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).
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478
Book Description
Transonic Aerodynamic Damping and Oscillatory Stability in Yaw and Pitch for a Model of a Variable-sweep Supersonic Transport Airplane
Author: Bruce R. Wright
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
Book Description
Keywords Index to U.S. Government Technical Reports
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 990
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 990
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
AIAA Aerodynamic Testing Conference, Washington, D.C., March 9-10, 1964
Author:
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 252
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 252
Book Description
Proceedings March 9-10, 1964
Author: AIAA Aerodynamic Testing Conference
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 258
Book Description
Keywords Index to U.S. Government Technical Reports (permuted Title Index).
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 522
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 522
Book Description
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
Book Description