Accession Number:

ADA055395

Title:

Progress Report on Analytic Investigation of Multinozzle Plume Flow Fields.

Descriptive Note:

Interim rept. 1 Oct 76-30 Sep 77,

Corporate Author:

GRUMMAN AEROSPACE CORP BETHPAGE N Y RESEARCH DEPT

Personal Author(s):

• Rudman,Stanley

Report Date:

1978-01-01

Pagination or Media Count:

22.0

Abstract:

Progress on the research effort Analytical Investigation of Multinozzle Plume Flow Fields includes major achievements such as the development of numerical techniques and a computer code for calculation of the impingement of two rectangular plumes, and a parametric study indicating that near field shock heating due to multiple nozzle flow field impingement can explain experimental data. Author

Descriptors:

• *EXHAUST PLUMES
• *NOZZLE GAS FLOW
• STATE OF THE ART
• SHOCK WAVES
• FLOW FIELDS
• HEATING
• NUMERICAL METHODS AND PROCEDURES
• MACHINE CODING
• THREE DIMENSIONAL FLOW
• AIRCRAFT EXHAUST
• ROCKET EXHAUST
• IMPINGEMENT

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE