NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Conceptual Final Paper on the Preliminary Design of an Oblique Flying Wing SSTA conceptual Oblique Flying Wing Supersonic Transport Aircraft (OFW, or surfplane because of its shape) was first proposed in 1957. It was reintroduced in 1987 in view of the emerging technology of artificial stabilization. This paper is based on the performance and economics study of an M2 B747-100B replacement aircraft. In order to make a fair comparison of this configuration with the B747, an end-sixties structural technology level is assumed. It is shown that a modern stability and control system can balance the aircraft and smooth out gusts, and that the OFW configuration equals or outperforms the B747 in speed, economy and comfort.
Document ID
19880013507
Acquisition Source
Ames Research Center
Document Type
Contractor Report (CR)
Authors
Van der Velden, Alexander J. M.
(Van der Velden (Alexander J. M.) Berkeley, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 6, 1987
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-182879
NAS 1.26:182879
Report Number: NASA-CR-182879
Report Number: NAS 1.26:182879
Accession Number
88N22891
Funding Number(s)
CONTRACT_GRANT: NAG2-471
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available