NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Oblique wing supersonic transport conceptsThe economic and technical features of two SST concepts that offer the potential of reducing the impact of the environmental constraints on the aircraft design and performance are presented. The potential economic performance of these aircraft is referenced to equivalent passenger size subsonic designs employing consistent design guidelines and assumptions. Total operating cost and airline return on investment are utilized for the economic comparisons.
Document ID
19930029340
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Galloway, Thomas (NASA Ames Research Center Moffett Field, CA, United States)
Gelhausen, Paul (NASA Ames Research Center Moffett Field, CA, United States)
Moore, Mark (NASA Ames Research Center Moffett Field, CA, United States)
Waters, Mark (Eloret Inst. Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-4230
Report Number: AIAA PAPER 92-4230
Meeting Information
Meeting: AIAA, Aircraft Design Systems Meeting
Location: Hilton Head Island, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AIAA
Accession Number
93A13337
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available