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Advanced supersonic transport propulsion and configuration technology improvementsThis paper presents the results of recent Douglas Aircraft Company integration studies for an advanced supersonic transport. The studies include technology improvements such as superplastic formed and diffusion-bonded titanium sandwich primary structure, composite secondary structure, bicone engine inlet, improved mechanical suppressors based on flight test data, improved aerodynamic efficiency based on wind tunnel test data, and updated performance for both variable-cycle and low-bypass-ratio engines. Technology development requirements for an economically viable and environmentally acceptable advanced supersonic transport are defined through these studies. A new Douglas Aircraft Company baseline supersonic transport designed to carry 350 passengers is defined for cost comparisons.
Document ID
19810056566
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rowe, W. T.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Welge, H. R.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Johnson, E. S.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Rochte, L. S.
(Douglas Aircraft Co. Long Beach, CA, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 81-1595
Meeting Information
Meeting: Joint Propulsion Conference
Location: Colorado Springs, CO
Country: US
Start Date: July 27, 1981
End Date: July 29, 1981
Sponsors: SAE, ASME, AIAA
Accession Number
81A40970
Funding Number(s)
CONTRACT_GRANT: NAS1-16147
Distribution Limits
Public
Copyright
Other

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