Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-Alpha

Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-Alpha PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723027574
Category :
Languages : en
Pages : 128

Get Book Here

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

Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-Alpha PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723027574
Category :
Languages : en
Pages : 128

Get Book Here

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]

Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-[alpha] PDF Author: Nelson Pedreiro
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 130

Get Book Here

Book Description


Journal of Aircraft

Journal of Aircraft PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760

Get Book Here

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1076

Get Book Here

Book Description


Low-Speed Wind Tunnel Testing

Low-Speed Wind Tunnel Testing PDF Author: Jewel B. Barlow
Publisher: John Wiley & Sons
ISBN: 0471557749
Category : Technology & Engineering
Languages : en
Pages : 738

Get Book Here

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

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1002

Get Book Here

Book Description


Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538

Get Book Here

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 444

Get Book Here

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1294

Get Book Here

Book Description


Research and Technology Objectives and Plans Summary (RTOPS)

Research and Technology Objectives and Plans Summary (RTOPS) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 192

Get Book Here

Book Description