Accession Number:

ADA030380

Title:

Development of Theoretical Models and Description of Computer Program. Volume I.

Descriptive Note:

Final rept.,

Corporate Author:

AUBURN UNIV ALA DEPT OF AEROSPACE ENGINEERING

Personal Author(s):

• Harwell,Kenneth E.

Report Date:

1976-09-15

Pagination or Media Count:

76.0

Abstract:

Numerical computer models for the prediction of aircraft and missile exhaust plume flow fields are described. The flow model is capable of treating multiple shock waves in the exhaust plume. An infrared computer model is described and typical results are presented for some typical missile exhaust plumes. Author

Descriptors:

• *COMPUTER PROGRAMS
• *COMPUTERIZED SIMULATION
• *INFRARED RADIATION
• *EXHAUST PLUMES
• GUIDED MISSILES
• MODELS
• SHOCK WAVES
• THEORY
• TURBULENCE
• FLOW FIELDS
• KINETIC ENERGY
• JET ENGINE EXHAUST

Subject Categories:

• Computer Programming and Software
• Infrared Detection and Detectors

Distribution Statement:

APPROVED FOR PUBLIC RELEASE