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...
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]
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
Journal of Aircraft
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1076
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1076
Book Description
Low-Speed Wind Tunnel Testing
Author: Jewel B. Barlow
Publisher: John Wiley & Sons
ISBN: 0471557749
Category : Technology & Engineering
Languages : en
Pages : 738
Book Description
A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
Publisher: John Wiley & Sons
ISBN: 0471557749
Category : Technology & Engineering
Languages : en
Pages : 738
Book Description
A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1002
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1002
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 444
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 444
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294
Book Description
Research and Technology Objectives and Plans Summary (RTOPS)
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 192
Book Description