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ACCURACY AND APPLICATION OF A SECOND- ORDER THEORY FOR THREE-DIMENSIONAL SUPERSONIC AND LOW HYPERSONIC UNSTEADY FLOWS AROUND A THIN WING
Qian Fuxing;Gu Weikai;He Longde
1981, (1): 1-9.
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EXPERIMENTAL INVESTIGATION ON INTERFERENCES OF TOP AND BOTTOM SLOTTED WALLS AND EFFECTS OF SIDE- WALLS IN A TRANSONIC AIRFOIL WIND TUNNEL
Research team on airfoil
1981, (1): 10-20.
THE BIPARAMETRIC CYCLE COUNT METHOD AND THE PRINCIPLE OF SIMPLIFICATION
Jiang Zuguo
1981, (1): 21-31.
A GENERAL FORMULA OF STRESS INTENSITY FACTORS FOR CT SPECIMENS
Wang Keren
1981, (1): 32-37.
A FINITE ELEMENT METHOD FOR LOCAL BUCKLING OF A STIFFENED PANEL IN AXIAL COMPRESSION
Liu Dongchang
1981, (1): 38-49.
TESTS FOR INLET DISTORTION IN A TWO-SPOOL TURBOJET ENGINE ON THE GROUND TEST BED
Jiang Feng
1981, (1): 59-68.
FUNDAMENTAL INVESTIGATION ON JET ENGINE IGNITION OF FUEL SPRAYS AND ITS APPLICATION
Chen Nengkun
1981, (1): 69-74.
DEVELOPMENT OF AN ASTRO-INERTIAL HYBRID NAVIGATION SYSTEM AND A STAR TRACKER
Shen Gongxun;Qin Shiguang;Chang Qingzhi;zhou Danian
1981, (1): 75-86.
MONOPULSE TECHNIQUE IN AIRBORNE RADAR
Ji Jie
1981, (1): 87-94.
MECHANISM OF STRESS CORROSION CRACKING AND HYDROGEN INDUCED CRACKING
Zhu Wuyang;Li Shiqiong;Xiao Jimei;Zhu Shuyan
1981, (1): 95-104.
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