Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
Book Description
Langley 14- by 22-foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual
Author: P. Frank Quinto
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1994
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1994
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1450
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1450
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 182
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 182
Book Description
User's Manual for the Langley Research Center 14- by 22- Foot Subsonic Tunnel Static Data Acquisition System
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Langley 14- By 22-Foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722611507
Category :
Languages : en
Pages : 64
Book Description
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircraft models. To support these investigations, a data acquisition system has been developed that has both static and dynamic capabilities. The static data acquisition and reduction system is described; the hardware and software of this system are explained. The theory and equations used to reduce the data obtained in the wind tunnel are presented; the computer code is not included. Quinto, P. Frank and Orie, Nettie M. Langley Research Center...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722611507
Category :
Languages : en
Pages : 64
Book Description
The Langley 14- by 22-Foot Subsonic Tunnel is used to test a large variety of aircraft and nonaircraft models. To support these investigations, a data acquisition system has been developed that has both static and dynamic capabilities. The static data acquisition and reduction system is described; the hardware and software of this system are explained. The theory and equations used to reduce the data obtained in the wind tunnel are presented; the computer code is not included. Quinto, P. Frank and Orie, Nettie M. Langley Research Center...
Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312)
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 392
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 392
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 88
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 88
Book Description
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1374
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1374
Book Description