Acta Mechanica Sinica (Selected Articles),

reportActive / Technical Report | Accession Number: ADA162726 | Open PDF

Abstract:

Contents Investigation of Rolling-up and Interaction of Leading-edge and Trailing-edge Vortex Sheets on a Slender Delta WIng Calculation of Circular Jet with Particles Impacting Upon a Plate A Non-local Elastic Plastic Continum Model and the Distress Distribution Near a Cracked Tip Study of Plane Stress with Elastic Plastic Mixed Node Fracture An Analytical Solution of Dynamic Response for Ideal Rigid Plastic General Variational Theorem for Structural Plastic Buckling Analysis Using Deformation Theory.

Author(s):
Yin, Xieyuan ; Xia, Nan ; Deng, Guohua ; Liu, Dayou ; Yu, Jilin
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Supplementary Note:
Edited trans. of Lixue Xuebao (China) n5 p454-475, 485-520 1984.
Annotation:
Acta Mechanica Sinica (Selected Articles)--Translation.
Pagination:
0125

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-ID(RS)T-0494-85
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_1.2.5_Lessons Learned; JCA_1.2.7_Experimentation; JCA_1.2.3_Educating; JCA_1.2.6_Concepts; JCA_4.6_Engineering
Communities of Interest:
Air Platforms
Descriptor(s):
*VORTICES, *BUCKLING, *JET FLOW, PLASTIC DEFORMATION, STRESSES, SLENDER BODIES, INTERACTIONS, STRUCTURAL ANALYSIS, DEFORMATION, DYNAMIC RESPONSE, THEORY, ELASTIC PROPERTIES, SOLUTIONS(GENERAL), SHEETS, TRANSLATIONS, LEADING EDGES, RIGIDITY, PLASTICS, DELTA WINGS, PLANE WAVES, CHINA, VARIATIONAL METHODS, ANALYTIC FUNCTIONS, TRAILING EDGES, CHINESE LANGUAGE, THEOREMS
Field(s)/Group(s):
Fluid Mechanics, Mechanics
Keyword(s):
Vortex sheets
Report Date:
1985 Dec 05