Author: Herbert S. GlickPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 172
Book Description
Flow Phenomena in Starting a Hypersonic Shock Tunnel
Author: Herbert S. GlickPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 172
Book Description
The High Temperature Aspects of Hypersonic Flow
Author: Wilbur C. NelsonPublisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
Book Description
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
A Perfect-gas Analysis of the Expansion Tunnel
Author: Robert L. TrimpiPublisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 116
Book Description
A perfect-gas analysis is presented for an apparatus consisting of a basic expansion tube at the downstream end of which a nozzle has been added. The resultant tube at the downstream end of which a nozzle has been added. The resultant apparatus, named the expansion tunnel, is shown to have the following advantages when compared with the basic expansion tube: increased testing time, larger initial test-gas slug length, higher efficiency, and reduced secondary-diaphgram bursting problems. Principal disadvantages are requirement of an additional nozzle, and the requirement disadvantages are requirement of an additional nozzle, and the requirement of a larger ratio between maximum and minimum pressures in an operating cycle. Authors conclude inherent advantages more than compensate for disadvantages.
Study of High-density Hypervelocity Flows and Similitudes
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 320
Book Description
NASA Technical Note
Author: Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, MdPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
Book Description
Handbook of Supersonic Aerodynamics
Author: I. I. GlassPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
Book Description
Hypersonic Research in the Shock Tunnel
Author: Charles E. WittliffPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 118
Book Description
Shock Tubes
Author: Irving Israel GlassPublisher: University of Toronto Press
ISBN: 1487597584
Category : Education
Languages : en
Pages : 983
Book Description
This volume contains the proceedings of a symposium held at the University of Toronto in June 1969. The symposium consisted of six sessions; each containing an invited paper, followed by six contributed papers reporting on recent, relevant research and development. The topics are: a review of research problems in basic shock tube flows and the possibilities for the shock tube in the future; driving techniques; explosive drivers; theoretical and experimental research in electromagnetic shock tubes; chemical kinetics and spectroscopy; and a review of shock tube diagnostics, instrumentation and fundamental data as well as the measurement of physical quantities.
Author: