Instrumentation of the Ames Supersonic Free-flight Wind Tunnel
Author : Robert O. Briggs
Publisher :
Page : 52 pages
File Size : 48,95 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : Robert O. Briggs
Publisher :
Page : 52 pages
File Size : 48,95 MB
Release : 1952
Category : Aeronautics
ISBN :
Author : Alvin Seiff
Publisher :
Page : 30 pages
File Size : 50,28 MB
Release : 1952
Category : Aerodynamics, Supersonic
ISBN :
Author : Clarence W. Matthews
Publisher :
Page : 320 pages
File Size : 42,56 MB
Release : 1955
Category : Aeronautics
ISBN :
Author : Michael Witunski
Publisher :
Page : pages
File Size : 18,30 MB
Release : 1948
Category :
ISBN :
Author :
Publisher :
Page : 750 pages
File Size : 47,82 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 568 pages
File Size : 10,65 MB
Release : 1951
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 258 pages
File Size : 36,2 MB
Release : 1953
Category : Aeronautics
ISBN :
Author : R. J. VOLLUZ
Publisher :
Page : 1 pages
File Size : 16,78 MB
Release : 1961
Category :
ISBN :
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 54 pages
File Size : 31,78 MB
Release : 2018-09-20
Category : Science
ISBN : 9781723862748
This manual describes the NASA Glenn Research Center's 1 - by 1 -Foot Supersonic Wind Tunnel and provides information for customers who wish to conduct experiments in this facility. Tunnel performance envelopes of total pressure, total temperature, and dynamic pressure as a function of test section Mach number are presented. For each Mach number, maps are presented of Reynolds number per foot as a function of the total air temperature at the test section inlet for constant total air pressure at the inlet. General support systems-such as the service air, combustion air, altitude exhaust system, auxiliary bleed system, model hydraulic system, schlieren system, model pressure-sensitive paint, and laser sheet system are discussed. In addition, instrumentation and data processing, acquisition systems are described, pretest meeting formats and schedules are outlined, and customer responsibilities and personnel safety are addressed.Seablom, Kirk D. and Soeder, Ronald H. and Stark, David E. and Leone, John F. X. and Henry, Michael W.Glenn Research CenterMACH NUMBER; REYNOLDS NUMBER; SUPERSONIC WIND TUNNELS; SUPERSONIC FLOW; TEST CHAMBERS; DATA ACQUISITION; MANUALS; WIND TUNNEL NOZZLES; DYNAMIC PRESSURE; WIND TUNNEL TESTS
Author : David E. Hahne
Publisher :
Page : 68 pages
File Size : 24,50 MB
Release : 1993
Category : Stability of airplanes
ISBN :