Author: Ying-Nien YuPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 186
Book Description
A Summary of Design Techniques for Axisymmetric Hypersonic Wind Tunnels
Author: Ying-Nien YuPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 186
Book Description
Handbook of Supersonic Aerodynamics
Author: George RudingerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 452
Book Description
Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics LaboratoryPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 460
Book Description
Technical Report - Jet Propulsion Laboratory, California Institute of Technology
Author: Jet Propulsion Laboratory (U.S.)Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 738
Book Description
Boundary-layer Characteristics at Mach Numbers 2 Through 5 in the Test Section of the 12-inch Supersonic Tunnel
Author: D. R. BellPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 44
Book Description
As part of a general tunnel calibration program, an investigation was made of the boundary-layer characteristics at Mach numbers 2, 3, 4, and 5 in the test section of the 12-Inch Supersonic Tunnel (D). The boundary-layer measurements were made at one longitudinal station (near the pitch sector center of rotation) on the centerline of both the flexible plate and sidewall. Measurements were also made at vertical locations on the sidewall between the sidewall centerline and the upper flexible plate. The boundary-layer total thickness, displacement thickness, and momentum thickness, are presented at each Mach number over a Reynolds number range corresponding, in general, to tunnel stagnation pressures between 5 and 60 psia. At each Mach number, the variation of displacement thickness on the side wall between the centerline and the upper flexible plate is presented as is a correlation of the flexible plate displacement thickness with experimental data obtained in other wind tunnels. Velocity profiles and test section Mach numbers are presented to indicate variations with Reynolds number.
Advances in Aeronautical Sciences
Author: Th. Von KármánPublisher: Elsevier
ISBN: 1483223353
Category : Technology & Engineering
Languages : en
Pages : 573
Book Description
Advances in Aeronautical Sciences, Volume 1 contains the proceedings of the First International Congress in the Aeronautical Sciences, held in Madrid, Spain in September 1958. The book is comprised of survey papers and original contributions that discuss common problems in aeronautics and in space technology. The reader will also find interesting articles that cover topics on the principles of inertial guidance; boundary layer control; VTOL/STOL aircraft; heat resisting material; heat transfer and heat barrier; and jet noises and human factors in aeronautics. Hypersonic speeds; propulsion methods in space and magneto-fluid dynamics are discussed as well. Aeronautics engineers and scientists in allied fields will find the book insightful.
Catalog of Books and Reports in the Bureau of Mines Technical Library, Pittsburgh, Pa
Author: United States. Bureau of Mines. Technical Library, PittsburghPublisher:
ISBN:
Category : Library catalogs
Languages : en
Pages : 778
Book Description
Technical Report
Author: Aeronautical Research Council (Great Britain)Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 802
Book Description
Includes its Reports, which are also issued separately.
National Union Catalog
Author: Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 728
Book Description
Includes entries for maps and atlases
ARS Journal
Author: American Rocket SocietyPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 1254
Book Description
Supplements accompany some issues.