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Effects of lengthwise lift distribution on sonic boom of SST configurations.Sonic boom signatures produced by diverse SST configurations during cruise, indicating aircraft length as overpressure limit factor
Document ID
19690065672
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ferri, A.
Ismail, A.
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Subject Category
Aircraft
Accession Number
69A43661
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-119
Distribution Limits
Public
Copyright
Other

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