Transonic Aerodynamics

reportActive / Technical Report | Accession Number: ADA207109 | Open PDF

Abstract:

A study has been made of finite span wings flying at the speed of sound. The general form of inner and outer expansions in terms of B reduced aspect ratio has been deduced. Suitable far field and near field expansions have been constructed and matched asymptotically. A new integral formula for the essential physical scale of the problem has been derived.

Author(s):
Cole, Julian ; Cook, L. P. ; Ziegler, F.
Author Organization(s):
CALIFORNIA UNIV LOS ANGELES DEPT OF MATHEMATICS
Descriptive Note:
Final rept.
Supplementary Note:
DOI: 10.21236/ADA207109
Pagination:
0002

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-89-0516
Contract/Grant Number(s):
F49620-79-C-0162
Task Number(s):
A4
Project Number(s):
2304
Monitor Series:
TR-89-0516, AFOSR
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*WINGS, *TRANSONIC FLOW, SCALE, TRANSONIC CHARACTERISTICS, ASPECT RATIO, AERODYNAMICS, FORMULAS(MATHEMATICS), FAR FIELD, PHYSICAL PROPERTIES, NEAR FIELD
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
FINITE SPAN WINGS, PE61102F, WUAFOSR2304A4
Report Date:
1980 Aug 01