Sonic boom reduction through aircraft design and operation.Means of reducing or eliminating the sonic boom through aerodynamic design or aircraft operation are discussed. These include designing aircraft to minimize or eliminate certain features of the overpressure signature, operating aircraft at slightly supersonic speeds so that the sonic boom does not reach the ground, and seeking reductions through the high altitude-high speed flight conditions of hypersonic transports.
Document ID
19730032864
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seebass, A. R.
George, A. R. (Cornell University Ithaca, N.Y., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 73-241Report Number: AIAA PAPER 73-241
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 10, 1973
End Date: January 12, 1973
Sponsors: American Institute of Aeronautics and Astronautics