NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
III. Supersonic cruise aircraftThe aviation world is on the threshold of sustained supersonic flight at a level of efficiency approaching the best of our subsonic aircraft. This potential has been recognized in the concept of the B-70. Now the supersonic transport is on the horizon. The supersonic transport represents a great technical challenge. Not only must this vehicle have the aerodynamic efficiency of the subsonic bomber, but it must also embrace: (a) the overriding element of passenger safety, (b) the problem of community acceptance (noise), and (c) economy of operation. This paper will be devoted primarily to the aerodynamic problems of large supersonic aircraft as related to performance. Smaller vehicles have been considered in part II of this compilation. The stability and control problems are of equal importance but are not discussed herein.
Document ID
19670023744
Acquisition Source
Headquarters
Document Type
Other - Technical Report
Authors
Donald D Baals
(Langley Research Center Hampton, Virginia, United States)
Cornelius Driver
(Langley Research Center Hampton, Virginia, United States)
Owen G Morris
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 3, 2013
Publication Date
October 1, 1960
Publication Information
Publication: Compilation of Papers Summarizing Some Recent NASA Research on Manned Military Aircraft
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: National Meeting on the Future of Manned Military Aircraft
Location: San Diego, CA
Country: US
Start Date: August 1, 1960
End Date: August 3, 1960
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
67N33073
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Supersonic aircraft
Problem solving
Aerodynamic characteristics
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available