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Thursday, May 7, 2020 | History

3 edition of Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds found in the catalog.

Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds

Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds

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Published by National Aeronautics and Space Administration, Ames Research Center, National Technical Information Service, distributor in [Moffett Field, Calif.], [Springfield, Va .
Written in English

    Subjects:
  • Aerodynamics, Hypersonic.,
  • Jet nozzles.

  • Edition Notes

    StatementEarl R. Keener.
    SeriesNASA-CR -- 187316., NASA contractor report -- NASA CR-187316.
    ContributionsAmes Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15368282M

    Schneider, S.P.: Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds. J. of Spacecraft and Rockets 36(1), 8–20 () CrossRef Google Scholar Author: Ernst Heinrich Hirschel. PUBLISHES A NEW BOOK The book, Global Formulations of Lagrangian and Hamiltonian Dynamics on Manifolds, authored by Taeyoung Lee, Melvin Leok and N. Harris McClamroch, is based on aspects of the doctoral research of Taeyoung Lee from – carried out at the U-M Department of Aerospace Engineering.

    United States. National Aeronautics and Space Administration: Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds / (Washington, DC: U.S. G.P.O., ), also by Vernon Van Hise and Langley Research Center (page images at HathiTrust) United States. Cengel and Cimbala's Fluid Mechanics Fundamentals and Applications, communicates directly with tomorrow's engineers in a simple yet precise manner, while covering the basic principles and equations of fluid mechanics in the context of numerous and .

    Exobiology Program Office NASA An Experimental Comparison of Two Designs of Mercury Propellant Cork R B Tank for use with an Electric Propulsion Engine (Ion Propulsion Box 1) An Experimental Investigation of Base Heating on Typical Mars Entry Zappa O L and Reinecke W G Body Shapes An Experimental Study of Visual Detection in a Spacecraft. Karen S. Green and Terrill W. Putnam, “Measurements of Sonic Booms Generated by an Airplane Flying at Mach and ,” NASA TM-X (October ). (Since hypersonic speeds were not directly relevant for the SST, a formal report was delayed until NASA began planning re-entry flights by the Space Shuttle.).


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Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds Download PDF EPUB FB2

Get this from a library. Experimental research of the aerodynamics of nozzles and plumes at hypersonic speeds. [Earl R Keener; Ames Research Center.]. Experimental Hypersonic Aerodynamic Characteristics of the Mars Surveyor Precision Lander with Flap Thomas J.

Horvath ∗, Tod F. O Connell ⊕. Benchmark CFD Study of Spiked Blunt Body Configurations. Experimental research of the aerodynamics of nozzles and plumes at hypersonic : Roberto Roveda. Hypersonic Nozzle-Afterbody Experiment: Flow-field Surveys A Experimental Investigation of Side-Jet Steering for Supersonic and Hypersonic Missiles A Experimental and Numerical Study of Hyperson-ic Forward-Facing Cavity Flow A Compressibility and Pressure-Gradient Correc-tion Assessment for Turbulent Hypersonic Flows A For the purpose of discussion, the facility 1 requirement in this report are divided into the following categories: subsonic and supersonic airplane systems, turbopropulsion systems, hypersonic and transatmospheric systems, and launch and space systems.

In general, the committee describes needs in which technology is a driving factor and certain system developments appear likely.

A supersonic transport (SST) is a civil aircraft designed to transport passengers at speeds greater than the speed of sound. The only supersonic civilian aircraft to see service are the Soviet produced Tupolev Tu which first flew in and was retired inand the Franco-British produced Concorde, which first flew in and remained.

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Numerical and Experimental Research of 3D Intake for Cruise Supersonic Business Aircraft.

Vladimir Stepanov, Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material Part 1: Experimental Results. Conceptual Design of Short Takeoff Supersonic Aircraft with Cold Flow Nozzles Vignesh. M 1, Sathish. K1, Adrin Issai Arasu.

L1, Dharun Lingam. K1, and Sanal Kumar. V.R 2 consumption and poor range) in turn making it unprofitable for manufacturers to produce these kinds of aircraft. It can cover a distance from India to USA in 2 ½ hours.

Summarizing these studies, the design of the ARCC engine powered SSTO vehicle are stated in the Chapter 3 as Configuration and planform, Wings, Takeoff and Landing, Numerical Vehicle, Mass Properties, and Aerodynamics including Interfering.

NASA Images Solar System Collection Ames Research Center. Brooklyn Museum. Full text of "NASA Technical Reports Server (NTRS) Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft, volume 1". Analysis of turbulent flows Tuncer Cebeci. Modelling and Computation of Turbulent Flows has been written by one of the most prolific authors in the field of CFD.

Professor of aerodynamics at SUPAERO and director of DMAE at ONERA, the author calls on both his academic and industrial experience when presenting this work. making this book. Gas dynamics deals with the flow of fluids that undergo significant density changes, such as the flow of gases through nozzles at high speeds.

The category aerodynamics deals with the flow of. NASA Images Solar System Collection Ames Research Center. Brooklyn Museum. Full text of "NASA Technical Reports Server (NTRS) RCS jet-flow field interaction effects on the aerodynamics of the space shuttle orbiter" See other formats.

Gas dynamics deals with the flow of fluids that undergo significant density changes, such as the flow of gases through nozzles at high speeds.

The category aerodynamics deals with the flow of gases (especially air) over bodies such as aircraft, rockets, and automobiles at high or low speeds.

Professor Kontis is a world-leading authority in aerospace engineering including integrated wing technologies, air-transport systems and space access, and multi-disciplinary applications of aerodynamics, shock physics, wind tunnel testing, flow control and diagnostics.

He has published more than articles including in journals, 6 book. PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone) Richard C. Klein [email protected] East 9th Street # Cleveland, OH () U.S.

Citizen or Legal Resident: Yes TECHNICAL ABSTRACT (LIMIT. Brazier, Jean-Philippe und Martinez Schramm, Jan und Paris, Sébastien und Gawehn, Thomas () An overview of HyFIE Technical Research Project: cross testing in main European hypersonic wind tunnels on EXPERT body. 50th 3AF International Conference on Applied Aerodynamics, -   The jets can be classified based on either pressure or Mach number prevalent at the exit of a nozzle or orifice.

The jets can be broadly classified into incompressible and compressible jets. The jets with Mach number less than till which the compressibility effects are ignored are called incompressible jets.

The Online Books Page. Online Books by. Langley Research Center. A Wikipedia article about this author is available. Langley Research Center: A Computer Program for the Determination of the Acoustic Pressure Signature of Helicopter Rotors Due to Blade Thickness (NASA Technical Memorandum X; ), also by Gerald H.

Mall and F. Farassat (page images at HathiTrust). Computational and Experimental Investigation of the Aerodynamics of Unconventional W Wings Musaj, M. / Prince, S. / Cheung, C.-W. / American Institute. NASA Glenn Research Center. 8 Curr an, E.

T., Sc ramjet Propulsion AIAA, ISBN 1 4, 9 Roudakov, A., Semenov, V., Kopchenov, V., Hicks, J. Future Flight Test Plans of an Axisymmetric Hydrogen Fueled Scramjet Engine on the Hypersonic Flying Laboratory AIAA 96 7 th Intern ational Spaceplanes and Hypersonics Systems.() Sinking, merging and stationary plumes in a coupled chemotaxis-fluid model: a high-resolution numerical approach.

Journal of Fluid Mechanics() Simulation of shock wave diffraction by a square cylinder in gases of arbitrary statistics using a semiclassical Boltzmann–Bhatnagar–Gross–Krook equation by: Configuration development study of the XC hypersonic research airplane. NASA Factsheet FSDFRC X NASA Factsheet FSDFRC X NASA Factsheet FSDFRC X NASA Factsheet FSDFRC X NASA Factsheet FSDFRC X Hyper-X.