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LIFTING SURFACE THEORY AND THE NUMERICAL METHOD OF WINGS WITH SMALL ANGLES OF SIDESLIP AT SUBSONIC AND SUPERSONIC SPEEDS
Huang Mingke
1980, (2): 1-10.
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SECOND-ORDER THREE-LEVEL SCHEME FOR TIME-DEPENDENT FINITE DIFFERENCE METHODS
Hou Tiansiang;Zhou Rangchun;Meng Dejun
1980, (2): 11-21.
CALCULATION OF NONLINEAR COMPRESSIBILITY EFFECTS OF AIRFOILS IN SUBCRITICAL CONDITIONS
Bei Xizeng
1980, (2): 22-17.
SUPERMATRIX METHOD FOR MULTI-SUBSTRUCTURE ANALYSIS
Yue Zhongdi
1980, (2): 28-35.
CONFORMING ELEMENT WITH OUT-ELEMENT NODES
Wang Shoumei
1980, (2): 36-44.
THE DIGITAL SIMULATION OF STABILITY FOR MULTI-STAGE AXIAL COMPRESSOR
Tang Diyi;Li Wenlan;Cong Mengzi
1980, (2): 52-61.
AN APPROACH OF INCREASING LIQUID ROCKET ENGINE PERFORMANCE--STUDY ON HEAT FLUX REDUCTION IN N_2O_4-UDMH ENGINE
Pan Shian
1980, (2): 62-66.
ON THE APPROXIMATE AND EXACT SOLUTIONS OF HIGH ORDER CHARACTERISTIC POLYNOMIAL AND ITS APPLICATION IN SOLVING ROOT-LOCUS EQUATION IN A CLOSED-LOOP SERVOMECHANISM
Lin Shinge
1980, (2): 67-78.
ELECTROMAGNETIC WAVE ABSORBERS AND THEIR APPLICATION TO AERONAUTICAL ENGINEERING
Wu Dawei
1980, (2): 79-88.
THE INVESTIGATION ON THE MICROSTRUCTURE STABILITY OF CAST NICKEL-BASE SUPERALLOY K002 AND K19H
Cat Yulin;Zheng Yunrong
1980, (2): 89-98.
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