Author: Nelson Pedreiro
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 130
Book Description
Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-[alpha]
Author: Nelson Pedreiro
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 130
Book Description
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 130
Book Description
Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-Alpha
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723027574
Category :
Languages : en
Pages : 128
Book Description
A unique experimental apparatus that allows a wind tunnel model two degrees of freedom has been designed and built. The apparatus was developed to investigate the use of new methods to augment aircraft control in the high angle of attack regime. The model support system provides a platform in which the roll-yaw coupling at high angles of attack can be studied in a controlled environment. Active cancellation of external effects is used to provide a system in which the dynamics are dominated by the aerodynamic loads acting on the wind tunnel model. Pedreiro, Nelson Ames Research Center WIND TUNNEL TESTS; AIRCRAFT CONTROL; AERODYNAMIC LOADS; ACTIVE CONTROL; WIND TUNNEL STABILITY TESTS; AERODYNAMIC STABILITY; WIND TUNNEL APPARATUS; WIND TUNNEL MODELS; DEGREES OF FREEDOM; ANGLE OF ATTACK; FLOW DISTRIBUTION...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723027574
Category :
Languages : en
Pages : 128
Book Description
A unique experimental apparatus that allows a wind tunnel model two degrees of freedom has been designed and built. The apparatus was developed to investigate the use of new methods to augment aircraft control in the high angle of attack regime. The model support system provides a platform in which the roll-yaw coupling at high angles of attack can be studied in a controlled environment. Active cancellation of external effects is used to provide a system in which the dynamics are dominated by the aerodynamic loads acting on the wind tunnel model. Pedreiro, Nelson Ames Research Center WIND TUNNEL TESTS; AIRCRAFT CONTROL; AERODYNAMIC LOADS; ACTIVE CONTROL; WIND TUNNEL STABILITY TESTS; AERODYNAMIC STABILITY; WIND TUNNEL APPARATUS; WIND TUNNEL MODELS; DEGREES OF FREEDOM; ANGLE OF ATTACK; FLOW DISTRIBUTION...
Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-alpha ... Nasa-cr-203760 ... Jun. 23, 1997
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Longitudinal Airplane Dynamics Wind Tunnel Test Equipment
Author: O. B. Tufts
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246
Book Description
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246
Book Description
Evaluation of a Novel Experimental Apparatus for Dynamic Wind Tunnel Testing
Author: Ihssane Mounir
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Wind Tunnel Test Techniques
Author: Colin Britcher
Publisher: Academic Press
ISBN: 0128181001
Category : Technology & Engineering
Languages : en
Pages : 672
Book Description
Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Publisher: Academic Press
ISBN: 0128181001
Category : Technology & Engineering
Languages : en
Pages : 672
Book Description
Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Journal of Aircraft
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760
Book Description
Apollo Wind Tunnel Testing Program
Author: William C. Moseley (Jr.)
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 84
Book Description
Measurement of Dynamic Stability Derivatives in the Wind Tunnel
Author: O. B. Tufts
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 126
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 126
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 892
Book Description