Accession Number:

ADA038614

Title:

Supersonic Jet Exhaust Noise Investigation. Volume III. Computer User's Manual for Aero-Acoustic Predictions.

Descriptive Note:

Final technical rept. 1 Dec 72-23 Sep 75,

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OHIO AIRCRAFT ENGINE GROUP

Report Date:

1976-07-01

Pagination or Media Count:

683.0

Abstract:

This report gives a detailed description of aerodynamic Shock-freeShocked flow and acoustic turbulent mixing computer prediction programs developed by the General Electric Company for subsonic and supersonic simple exhaust jets. In addition to giving detailed descriptions of the aeroacoustic formulations and discussions of computer manual instructions for operating the program, extensive theorydata comparisons are given, as well as computer program listings and sample test cases. Author

Subject Categories:

  • Acoustics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE