DETERMINATION OF THE PROFILE OF LEAST RESISTANCE OF AN ANNULAR WING

reportActive / Technical Report | Accession Number: AD0410936 | Open PDF

Abstract:

A thin axisymmetric wing in a supersonic flow is studied to determine the profile of least resistance of an annular wing.

Author(s):
Borisov, B. I.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Supplementary Note:
Trans. from Vestnik Moskovskogo Universiteta, No. 1, pp. 62-65, 1961.
Annotation:
DETERMINATION OF THE PROFILE OF LEAST RESISTANCE OF AN ANNULAR WING -- Translation.
Pagination:
0010

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):
FTD-TT-63-397
Monitor Series:
FTD
 Subject Terms
Joint Capability Areas:
JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support
Communities of Interest:
Air Platforms
Descriptor(s):
*RING WINGS, AERODYNAMIC DRAG, RUSSIA, TRANSLATIONS, SUPERSONIC CHARACTERISTICS
Field(s)/Group(s):
Aerodynamics
Keyword(s):
FOREIGN REPORTS
Report Date:
1963 Jun 11