NDLI: Results of convective heating tests of a longitudinal gap on the rockwell flat plate model (15-0, insert 7) in the nasa/ames research center

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Results of convective heating tests of a longitudinal gap on the rockwell flat plate model (15-0, insert 7) in the nasa/ames research center

Content Provider	NASA Technical Reports Server (NTRS)
Author	Quan, M. Lockman, W. K.
Copyright Year	1975
Description	Results are presented which were obtained from tests in a hypersonic wind tunnel to determine aerodynamic heating rates in a gap running parallel or slightly askew to the flow direction. The model used was a flat plate instrumented in thin-skin sections with chromelconstantan thermocouples. Heating rate profiles lengthwise along and down into the gap were obtained, and additional data were obtained from a total temperature probe and rake fabricated during the test to investigate an apparent aerodynamic cooling trend in the gap. Model variables were width, depth, length, and orientation of the gap relative to the flow direction. The tests were conducted at Mach 5.1 and Reynolds numbers per foot of 500,000, 1,000,000, and 2,000,000.
File Size	918606296
Page Count	416
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19750022163
Archival Resource Key	ark:/13960/t5z659f3t
Language	English
Publisher Date	1975-07-01
Access Restriction	Open
Subject Keyword	Spacecraft Design, Testing And Performance Convective Heat Transfer Tables Data Hypersonic Speed Flat Plates Thermocouples Reynolds Number Wind Tunnel Tests Hypersonic Wind Tunnels Wind Tunnel Models Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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