Sonic-boom calculation in a stratified atmosphere.For a lifting body of revolution, the exact solutions to the gas dynamical equation are given for the flow field in a stratified atmosphere. The boundary condition is satisfied by using the (linearized) slender-body theory. The solution allows one to make a prediction of the magnitude and the location of the sonic boom in a stratified atmosphere as well as to handle cutoff effects.
Document ID
19720045919
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Schorling, M. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Aircraft
Meeting Information
Meeting: Noise and vibration control engineering; Purdue Noise Control Conference