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Design feasibility of an advanced technology supersonic cruise aircraftResearch and development programs provide confidence that technology is in-hand to design an economically attractive, environmentally sound supersonic cruise aircraft for commercial operations. The principal results of studies and tests are described including those which define the selection of significant design features. These typically include the results of: (1) wind-tunnel tests, both subsonic and supersonic, (2) propulsion performance and acoustic tests on noise suppressors, including forward-flight effects, (3) studies of engine/airframe integration, which lead to the selection of engine cycles/sizes to meet future market, economic, and social requirements; and (4) structural testing.
Document ID
19770011096
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rowe, W. T.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Proc. of the SCAR Conf., Pt. 2,
Subject Category
Aircraft Design, Testing And Performance
Accession Number
77N18040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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