Transonic Flow Research

reportActive / Technical Report | Accession Number: ADA215096 | Open PDF

Abstract:

Topics study include Fictitious gas designed method Conical flow Unsteady transonic flow computations with input pressure distributions Unsteady wind tunnel interference and Inviscid flow with shock induced vorticity. edc

Author(s):
Fung, K. Y.
Author Organization(s):
ARIZONA UNIV TUCSON DEPT OF AEROSPACE AND MECHANICAL ENGINEERING
Descriptive Note:
Final rept. 1 Feb 1981-30 Jun 1982,
Supplementary Note:
DOI: 10.21236/ADA215096
Pagination:
0006

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFOSR-TR-89-1548
Contract/Grant Number(s):
AFOSR-81-0107
Task Number(s):
A1
Project Number(s):
2307
Monitor Series:
TR-89-1548, AFOSR
 Subject Terms
Joint Capability Areas:
JCA_1.2_Force Preparation; JCA_1_Force Support
Communities of Interest:
Air Platforms
Descriptor(s):
*TRANSONIC FLOW, COMPUTATIONS, VORTICES, SHOCK, WIND TUNNEL TESTS, FLOW, UNSTEADY FLOW, INVISCID FLOW, PRESSURE DISTRIBUTION, INPUT, INTERFERENCE
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
CONICAL FLOW, PE61102F, WUAFOSR2307A1
Report Date:
1982 Dec 01