NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Transonic transport study, summaryThe effects of possible increases in cruise speed over present-day transport aircraft were investigated. Increased cruise speed is desirable not only because of a possible competitive market advantage, but also because of the resulting increase in aircraft productivity. Aircraft designed to cruise at Mach numbers greater than those of present-day transports but less than those which produce a sonic boom on the ground were studied. The purpose of the study was three-fold: (1) to compare, on an equal basis, the performance and economics of advanced commercial transport aircraft designed to cruise at Mach numbers 0.90, 0.98, and 1.15; (2) to determine the sensitive technical areas affecting the performance and economics of the aircraft; and (3) to assess the impact of advanced technology, particularly the supercritical wing and advanced composite materials on the performance and economics of the aircraft.
Document ID
19720018359
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Williams, L. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62156
Report Number: NASA-TM-X-62156
Accession Number
72N26009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available