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The Leading Edge 250: Oblique wing aircraft configuration project, volume 4The design of a high speed transport aircraft using the oblique wing concept as a part of the High Speed Civil Transport (HSCT) aircraft study is the Leading Edge 250 capable of travelling at Mach 4 with 250 passengers and has a 6,500 nautical mile range. Its innovation lies within its use of the unconventional oblique wing to provide efficient flight at any Mach number. Wave drag is kept to a minimum at high speed, while high lift is attained during critical takeoff and landing maneuvers by varying the sweep of the wing.
Document ID
19890009039
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schmidt, Andre
(California State Polytechnic Univ. Pomona, CA, United States)
Moore, Peri
(California State Polytechnic Univ. Pomona, CA, United States)
Nguyen, Dan
(California State Polytechnic Univ. Pomona, CA, United States)
Oganesyan, Petros
(California State Polytechnic Univ. Pomona, CA, United States)
Palmer, Charles
(California State Polytechnic Univ. Pomona, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 11, 1988
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.26:184702
NASA-CR-184702
Report Number: NAS 1.26:184702
Report Number: NASA-CR-184702
Accession Number
89N18410
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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