Characteristics of Double-Canard Aerodynamic Shape Configuration

reportActive / Technical Report | Accession Number: ADA128337 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Bao-xing, Wang
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Supplementary Note:
Edited trans. of Lixue yu Shuian (China) v2 n2 p26-30 1980.
Annotation:
Characteristics of Double-Canard Aerodynamic Shape Configuration -- Translation.
Pagination:
0016

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited. Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-ID(RS)T-0659-82
Monitor Series:
FTD
 Subject Terms
Joint Capability Areas:
JCA_3_Force Application; JCA_7.2.1_Mitigate Lethal Effects; JCA_7.2_Mitigate; JCA_7_Protection; JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
*AIR TO AIR MISSILES, TRANSLATIONS, LIFT, CHINA, AERODYNAMICS, CANARD CONFIGURATIONS
Field(s)/Group(s):
Air- and Space-Launched Guided Missiles, Fluid Mechanics
Keyword(s):
DOUBLE CANARDS, FOREIGN REPORTS
Report Date:
1983 Apr 06