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Slotted test section dynamics of the NTFA dynamic model of the National Transonic Facility (NTF) section and plenum chamber was developed. The model serves as a means for determining the dynamic performance of the NTF and the subsequent design of optimal control configurations, and is of one dimensional flow type as to facilitate computer simulation. The model allows for the simulation of the effects of test section blockage, boundary layer losses, slot flow required for supersonic flow generation, reentry flap position, and auxiliary plenum suction.
Document ID
19780004163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gumas, G.
(Pennsylvania State Univ. Middletown, PA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1977
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
REPT-1
NASA-CR-155266
Report Number: REPT-1
Report Number: NASA-CR-155266
Accession Number
78N12106
Funding Number(s)
CONTRACT_GRANT: NSG-1457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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