NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A computing method for sound propagation through a nonuniform jet streamThe classical formulation of sound propagation through a jet flow was found to be inadequate for computer solutions. Previous investigations selected the phase and amplitude of the acoustic pressure as dependent variables requiring the solution of a system of nonlinear algebraic equations. The nonlinearities complicated both the analysis and the computation. A reformulation of the convective wave equation in terms of a new set of dependent variables is developed with a special emphasis on its suitability for numerical solutions on fast computers. The technique is very attractive because the resulting equations are linear in nonwaving variables. The computer solution to such a linear system of algebraic equations may be obtained by well-defined and direct means which are conservative of computer time and storage space. Typical examples are illustrated and computational results are compared with available numerical and experimental data.
Document ID
19750043785
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Padula, S. L.
Liu, C. H.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1974
Subject Category
Aerodynamics
Meeting Information
Meeting: Acoustical Society of America, Meeting
Location: St. Louis, MO
Start Date: November 4, 1974
End Date: November 8, 1974
Sponsors: USAF
Accession Number
75A27857
Distribution Limits
Public
Copyright
Other

Available Downloads

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