Author: Virgil A. SandbornPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Measurements of Flow Duration in a Low-pressure Shock Tube
Author: Virgil A. SandbornPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
NASA Technical Note
Author: 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.
Technical Information Pilot
Author: Handbook of Supersonic Aerodynamics
Author: I. I. GlassPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
Book Description
A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification
Author: Robert L. TrimpiPublisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 674
Book Description
The nonlinear characteristic differential equations applicable to a quasi-one-dimensional unsteady channel flow with friction and heat transfer are linearized and integrated in functional form for the particular study of small perturbations from ideal shock-tube flows. If the equivalence of unsteady- and steady-flow boundary layers is assumed, the problem of determining the perturbation in the unsteady flow reduces to an evaluation of the drag of a flat plate in the equivalent steady flow.
Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, MdPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 642
Book Description
Application of Shock Tubes to Transonic Airfoil Testing at High Reynolds Numbers
Author: Shock Tubes and Waves
Author: Charles E. TreanorPublisher: SUNY Press
ISBN: 9780873955959
Category : Philosophy
Languages : en
Pages : 1130
Book Description
Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.
High Speed Problems of Aircraft and Experimental Methods
Author: Allen F. DonovanPublisher: Princeton University Press
ISBN: 140087503X
Category : Science
Languages : en
Pages : 1021
Book Description
Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.