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: Test Time in Low Pressure Shock Tubes
Author: Aerospace CorporationPublisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 86
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.
Scientific and Technical Aerospace Reports
Author: 30th International Symposium on Shock Waves 2
Author: Gabi Ben-DorPublisher: Springer
ISBN: 3319448668
Category : Technology & Engineering
Languages : en
Pages : 681
Book Description
These proceedings collect the papers presented at the 30th International Symposium on Shock Waves (ISSW30), which was held in Tel-Aviv Israel from July 19 to July 24, 2015. The Symposium was organized by Ortra Ltd. The ISSW30 focused on the state of knowledge of the following areas: Nozzle Flow, Supersonic and Hypersonic Flows with Shocks, Supersonic Jets, Chemical Kinetics, Chemical Reacting Flows, Detonation, Combustion, Ignition, Shock Wave Reflection and Interaction, Shock Wave Interaction with Obstacles, Shock Wave Interaction with Porous Media, Shock Wave Interaction with Granular Media, Shock Wave Interaction with Dusty Media, Plasma, Magnetohyrdrodynamics, Re-entry to Earth Atmosphere, Shock Waves in Rarefied Gases, Shock Waves in Condensed Matter (Solids and Liquids), Shock Waves in Dense Gases, Shock Wave Focusing, Richtmyer-Meshkov Instability, Shock Boundary Layer Interaction, Multiphase Flow, Blast Waves, Facilities, Flow Visualization, and Numerical Methods. The two volumes serve as a reference for the participants of the ISSW30 and anyone interested in these fields.
Experimental Study of the Equivalence of Transonic Flow about Slender Cone-cylinders of Circular and Elliptic Cross Section
Author: William A. PagePublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 668
Book Description
The results of the investigation suggest that at transonic speeds and at small angles of attack the calculation of all aerodynamic characteristics of slender, three-dimensional shapes can be made by use of transonic slender-body theory when the pressures on the equivalent body of revolution are Imown, either by experiment, or by an adequate nonlinear theory. From transonic slender-body theory it is deduced that the slenderness required for this application is the same as that required for the successful application of the transonic area rule.
Instrumentation and Measurements in Compressible Flows
Author: Mrinal KaushikPublisher: CRC Press
ISBN: 100099953X
Category : Technology & Engineering
Languages : en
Pages : 356
Book Description
Instrumentation and Measurements in Compressible Flows presents detailed information on experiments in compressible fluid flows including technical information pertaining to a wide variety of applications and the experimental basis for compressible flows. A step-by-step procedure is given to estimate the measurement errors as well as the uncertainty. Computational fluid dynamics data can be validated with the experimental results presented in the book. Further, it answers most pertinent queries related to conducting experiments and measuring the data at very high speeds. This volume also includes MATLAB® programs for selected topics. Features: Presents detailed coverage of instrumentation, measurements, and experiments in compressible flows Covers both experimental and applied aspects of gas dynamics Provides a real-time exposure to the modern supersonic and hypersonic wind tunnel applications Explains supersonic and hypersonic shock/boundary-layer interactions and their control Includes real-time experimental problems and their analysis This book is aimed at researchers and graduate students in aerospace and mechanical engineering.
Space Programs Summary
Author: Jet Propulsion Laboratory (U.S.)Publisher:
ISBN:
Category : Space flight
Languages : en
Pages : 278
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 454
Book Description