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Comparisons of in-flight F-111A inlet performance for on and off scheduled inlet geometry at Mach numbers of 0.68 to 2.18In-flight F-111 data on total and static pressure from left inlet during automatically scheduled and manually controlled off-schedule positioning of spike at Mach 0.68 to 2.18
Document ID
19710023735
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hughes, D. L. (NASA Flight Research Center Edwards, CA, United States)
Martin, R. A. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6490
H-654
Accession Number
71N33211
Funding Number(s)
CONTRACT_GRANT: 720-52-00-04-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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