Simulation of time-varying ascent loads on arrays of shuttle tiles in a large transonic tunnel
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Simulation of time-varying ascent loads on arrays of shuttle tiles in a large transonic tunnel

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

Subjects:

  • Reusable space vehicles,
  • Unsteady flow (Aerodynamics)

Book details:

Edition Notes

StatementPercy J. Bobbitt, C.L.W. Edwards, and Richard W. Barnwell
SeriesNASA technical memorandum -- 84529
ContributionsEdwards, C. L. W, Barnwell, Richard W, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
The Physical Object
Pagination48 p. :
Number of Pages48
ID Numbers
Open LibraryOL17977348M

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Get this from a library! Simulation of time-varying ascent loads on arrays of shuttle tiles in a large transonic tunnel. [Percy J Bobbitt; C L W Edwards; Richard W Barnwell; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.]. Buy Simulation of time-varying ascent loads on arrays of shuttle tiles in a large transonic tunnel (NASA technical memorandum) by Bobbitt, Percy J (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Percy J Bobbitt.   • In , combined wind tunnel and vibration shaker tests were conducted on two Shuttle structural panels to determine the effects of combined loads on the thermal protection system (TPS). • In , the simulation of time varying ascent loads on arrays of Shuttle tiles was : Langley Research Center. Simulation of Time-varying Ascent Loads on Arrays of Shuttle Times in a Large Transonic Tunnel (Building ) Space Shuttle Plume Analysis by George Maddrea Further Reading. Becker, John V. The Development of Winged Reentry Vehicles. Champine, Gloria. interview. Daugherty, Robert H. and Thomas J. Yager.

American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA for Shuttle Orbiter Thermal Protection System Components: High Density Tile, Low Density Tile, Densified Low Density Tile, and Strain Isolation Pad. NASATM, October 7. Bobbitt, Percy J.; Edwards, Clyde L. W.; and Barnwell, Richard W.: The 8 Simulation of Time Varying Ascent Loads on Arrays of Shuttle Tiles in a Large Transonic Wind Author: R. D. Springfield, P. L. Lawing. American Institute of Aeronautics and Astronautics 3 II. S4T Wind-Tunnel Model Description The S4T represents a supersonic transport concept that was the subject of study through the High Speed Research (HSR) program in the s The wind-tunnel model is an aeroelastically-scaled half-span model with multiple sensors and three actuated control surfaces (Fig 1) The wing, forward Ride File Size: KB. The space shuttle at work / (Washington, D.C.: Scientific and Technical Information Branch and Division of Public Affairs, National Aeronautics and Space Administration, ), by Howard Allaway, United States. National Aeronautics and Space Administration. Public Affairs Division, and United States.

Numerical simulation of unsteady flow hydraulics of Truckee River / ([Reno, Nev.]: Center for Water Resources Research, Desert Research Institute, University of Nevada System, ), by Vulli L. Gupta and Syed M. Afaq (page images at HathiTrust; US access only). 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Numerical simulation of bus aerodynamics on several classes of bridge decks Article (PDF Available) in Engineering Applications of Computational Fluid Mechanics 11(1) July with Large-eddy simulation is used to predict heat transfer in the separated and reattached flow regions downstream of a backward-facing step. Simulations were carried out at a Reynolds number of