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Three-Component Force Measurements on a Scramjet in a Reflected-Shock TunnelA three-component stress-wave force-balance for a large scramjet has been designed, calibrated and tested in the HYPULSE reflected shock tunnel at GASL Inc., New York. The scramjet model is over 3-foot long and weighs in excess of 90 Ibm. The stress-wave force-balance is comprised of three stress bars which are attached to the model. Calibration results indicate that the force balance responds well within about 1 ms and that the sensitivity of the balance to the distribution of load is not large. Results with and without fuel injection were obtained in the tunnel operated for Mach 7 and Mach 10 flight simulation. These tests showed the force-balance can resolve axial force increments due to combustion of about 40 lb in the presence of model lift forces of 500-700 lb.
Document ID
19990114850
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Tsai, C.-Y.
(General Applied Science Labs., Inc. Ronkonkoma, NY United States)
Bakos, R. J.
(General Applied Science Labs., Inc. Ronkonkoma, NY United States)
Mee, D. J.
(Queensland Univ. Brisbane, Australia)
Date Acquired
August 19, 2013
Publication Date
December 1, 1998
Publication Information
Publication: JANNAF Airbreathing Propulsion Subcommittee and 35th Combustion Subcommittee Meeting
Volume: 1
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NAS1-97027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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