Last edited by Zulugar
Thursday, April 30, 2020 | History

3 edition of Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment found in the catalog.

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment

  • 55 Want to read
  • 22 Currently reading

Published by National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor in Edwards, Calif, Springfield, VA .
Written in English

    Subjects:
  • Aerodynamic heating.,
  • Boundary layer transition.,
  • Finite element method.,
  • Thermal analysis.,
  • Hypersonic speed.,
  • Design analysis.

  • Edition Notes

    StatementLeslie Gong and W. Lance Richards.
    SeriesNASA/TM -- 1998-206555., NASA technical memorandum -- 206555.
    ContributionsRichards, W. Lance., NASA Dryden Flight Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15541774M


Share this book
You might also like
The most delectable history of Reynard the Fox

The most delectable history of Reynard the Fox

More bush leatherwork.

More bush leatherwork.

Uncertainty in remote sensing and GIS

Uncertainty in remote sensing and GIS

Arbitration agreement between the Government of the United Kingdom (acting on behalf of the ruler of Abu Dhabi and His Highness the Sultan Said bin Taimur) and the Government of Saudi Arabia, with exchange of notes.

Arbitration agreement between the Government of the United Kingdom (acting on behalf of the ruler of Abu Dhabi and His Highness the Sultan Said bin Taimur) and the Government of Saudi Arabia, with exchange of notes.

monuments of Ancient Rome as coin types

monuments of Ancient Rome as coin types

Protests of DMA Contract Award for Systems Engineering and Evaluation Support, U.S. GAO, August 3, 1995.

Protests of DMA Contract Award for Systems Engineering and Evaluation Support, U.S. GAO, August 3, 1995.

Rapport Sur LInstruction Publique, Fait Au Nom Du Comitede Constitution a LAssemblee Nationale

Rapport Sur LInstruction Publique, Fait Au Nom Du Comitede Constitution a LAssemblee Nationale

Modern roadmaking, with special reference to materials and plant, etc

Modern roadmaking, with special reference to materials and plant, etc

A catalogue of transportation concepts proposed for Metropolitan Toronto

A catalogue of transportation concepts proposed for Metropolitan Toronto

Jasper National Park

Jasper National Park

Photochemical and photophysical processes in naphthalene, chloroacetylene, and aniline

Photochemical and photophysical processes in naphthalene, chloroacetylene, and aniline

Lenition and fortition

Lenition and fortition

Multinational corporations, technology, and employment

Multinational corporations, technology, and employment

Techniques for plant electron microscopy [by] B.E. Juniper [and others].

Techniques for plant electron microscopy [by] B.E. Juniper [and others].

Twelfth night

Twelfth night

Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment Download PDF EPUB FB2

THERMAL ANALYSIS OF A METALLIC WING GLOVE FOR A MACH-8 BOUNDARY-LAYER EXPERIMENT Leslie Gong * and W. Lance Richards † NASA Dryden Flight Research Center Edwards, CA Abstract A metallic “glove” structure has been built and attached to the wing of the Pegasus space booster.

An experiment on the upper surface of the glove has been designed Cited by: 3. Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment (SuDoc NAS ) [Leslie Gong] on *FREE* shipping on qualifying offers.

Get this from a library. Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment. [Leslie Gong; W Lance Richards; NASA Dryden Flight Research Center.].

Buy Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment (SuDoc NAS ) by Gong, Leslie (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Leslie Gong.

Preparations for a boundary-layer transition experiment to be conducted on a future flight mission of the air-launched Pegasus ® rocket are underway. The experiment requires a flight-test article called a glove to be attached to the wing of the Mach-8 first-stage booster.

A three-dimensional, nonlinear finite-element analysis has beenCited by: 3. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA   Thermal Analysis of a Metallic Wing Glove for a Mach-8 Boundary Layer Experiment Proceedings at 7th AIAA∕ASME Joint Thermophysics and Heat Transfer Conference, AIAA, Albuquerque, New Mexico, June 15–Cited by:   Theory of Stagnation Point Heat Transfer in Dissociated Air.

Boundary-layer Separation Detection for a Cone at High Angle of Attack in Mach Flow with Pressure-Sensitive Paint. Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer by: Library of Congress Cataloging-in-Publication Data (Revised for vol.

8) NASA historical data book. (NASA SP- ) Vol. 1 is a republication of NASA historical data book, –/ Jane Van Nimmen and Leonard C. Bruno.

Vol. 8 in series: The NASA historical data book series. Includes bibliographical references and indexes. Boundary Layer. NASA Technical Reports Server (NTRS) Loitsianskii. The fundamental, practically the most important branch of the modern mechanics of a viscous fl.

Thermal transport processes in stable boundary layers. NASA Astrophysics Data System (ADS) Gutierrez, Walter; Araya, Guillermo; Kiliyanpilakkil, Praju; Basu, Sukanta; Ruiz-Columbi.

Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A cumulative index to a continuing bibliography" See other formats. This banner text can have markup.

web; books; video; audio; software; images; Toggle navigation. 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 Determinat. Finite-Element Analysis of a Mach-8 Flight Test Article Using Nonlinear Contact Elements_专业资料。A flight test article, called a glove, is required for a Mach-8 boundary-layer experiment to be conducted on a flight mission of the air-launched Pegasus space : For the further depth thermal analysis, we propose to use the one-dimensional transient heat transfer finite element model of Blosser [].

Stardust, Skipper [Fullmer ], and Pegasus XL Wing-Glove Experiment[Richards et al ]. “Design of a Flight Article for a Mach-8 Boundary-Layer Experiment," AIAAAIAA, November. The boundary layer is separated from the contour of a planes airfoil, or wing section, by only a few thousandths of an inch.

Air particles change from a smooth laminar flow near the leading edge to a turbulent flow toward the airfoils rear.2 Turbulent flow increases friction on an aircrafts skin and therefore increased surface heat while 5/5(1).

NASA Historical Data Book Vol. 8 - Free ebook download as PDF File .pdf), Text File .txt) or read book online for free. NASA earth science and space applications, aeronautics,technology and exploration, tracking and data acquisition/space operations, facilities and resources.

=/5(1). Seventh IUTAM Symposium on Laminar-Turbulent Transition IUTAM BOOKSERIES Volume 18 Series Editors G.M.L.

Gladwell, Un. Dedicated to the Preservation of Aerospace Technology. A Not-for Profit Corporation () Fax () e-mail: [email protected] World Wide Web:http// Bogie Street Palmdale, CA The image above is a reproduction of the mural commissioned by NASA Dryden and created by Robert T.

McCall,which is part of the visitor's lobby at the NASA Dryden. Ablating materials: ballistic missiles, Ames atmosphere entry simulator to determine properties () char-forming, analysis of performance () chars, hemispherical spectral emittance to ''K () evaluation of thermal protection materials at moderate heating rates and high to- tal heat loads () exposed to.

Abstract: The objective of the proposed work is to develop a unified and optimum numerical method for solving fluid-structure interaction problems. We propose to use an unstructured solution-adaptive topology for both fluid and structure, and to discretize the governing equations for both using a.

Expanding the Envelope upper wing caused the lateral center of pressure in biplane wings to spread outward and (at high angles of attack) forward compared to a wing tested as a monoplane Elliott Reid’s final research as an NACA employee appeared in print in September.