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SECOND ORDER APPROXIMATION METHOD FOR TRANSONIC FLOWS OVER SWEPT WINGS
Shen Keyang
1983, (4): 1-10.
PDF [ 518 K ]( 338 ) HTML
A NUMERICAL SOLUTION OF THE SHOCK-TURBULENT BOUNDARY LAYER INTERACTION OVER A COMPRESSION CORNER FOR SUPERSONIC FLOW
Cao Qipeng
1983, (4): 11-19.
PDF [ 462 K ]( 289 ) HTML
A TWO-DIMENSIONAL GENERALIZED J INTEGRAL OF MIXED MODE
Wu Shaofu;Zhang Xing
1983, (4): 20-31.
PDF [ 551 K ]( 1384 ) HTML
IMPROVEMENT OF THE FINITE ELEMENT METHOD FOR ROTOR BLADE DYNAMICS ANALYSIS AND INTERNAL FORCE CALCULATION
Liu Shoushen
1983, (4): 32-38.
PDF [ 426 K ]( 322 ) HTML
OPTIMUM DESIGN OF A LIFTING-SURFACE STRUCTURE WITH MULTIPLE CONTRAINTS BY INTUITIVE OPTIMALITY CRITERIA
Lin Li-ang penned
1983, (4): 39-47.
PDF [ 498 K ]( 339 ) HTML
A TRANSFER MATRIX-DIRECT INTEGRATION METHOD AND ITS APPLICATION
Gu Jialiu
1983, (4): 48-56.
PDF [ 461 K ]( 279 ) HTML
ESTIMATION PROBLEM OF TARGET MANEUVERING ACCELERATION IN THREE-DIMENSIONAL SPACE
Zhou Hongren
1983, (4): 57-69.
PDF [ 640 K ]( 380 ) HTML
AN OPTIMUM INTERCEPT GUIDANCE LAW WITH UNCERTAIN FACTORS
Wang Chaozhu
1983, (4): 70-77.
PDF [ 372 K ]( 350 ) HTML
STUDY ON DYNAMIC CHARACTERISTICS OF COCKPIT TEMPERATURE CONTROL SYSTEM
Yang Shaozeng;Wang Jun
1983, (4): 78-85.
PDF [ 393 K ]( 397 ) HTML
A STUDY ON TACTICS OF OPTIMUM ADVANCED CHANGE FOR FLIGHT CONTROL SYSTEM
Jiao Guoquan;Dong Zeqing
1983, (4): 86-94.
PDF [ 470 K ]( 418 ) HTML
FRACTURE TESTS OF TURBINE DISK WITH CRACKS AND THEIR FEATURES
Wang Baohua
1983, (4): 95-100.
PDF [ 996 K ]( 331 ) HTML
THEORETICAL SPECIFIC IMPULSE FOR TWO-PHASE FLOW IN NOZZLE OF ROCKET-RAMJET ENGINE——A SIMPLE ESTIMATION METHOD
Bi Shiguan
1983, (4): 101-104.
PDF [ 240 K ]( 413 ) HTML
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