1004-499X
2001 Issue 4
A SELECTING VARIABLES ALGORITHM BASING ON THE PRINCIPAL COMPONENT PARAMETER ESTIMATION
tong li ; zhou hai yin
tong li ; zhou hai yin
..............page:1-6
SIMULATION ANALYSIS OF HIGH VELOCITY PENETRATION INTO CONCRETE TARGET
wang dao rong ; sun yu xin ; guo yang
wang dao rong ; sun yu xin ; guo yang
..............page:7-11
A METHOD TO DETERMINE THE PARAMETERS OF THE MODEL FOR CONCRETE IMPACT AND DAMAGE
zhang feng guo ; li en zheng
zhang feng guo ; li en zheng
..............page:12-16,23
MODELING AND DYNAMIC ANALYSIS OF NITROGEN LAUNCHING SYSTEM
dai long cheng ; xuan yi min ; yin jian
dai long cheng ; xuan yi min ; yin jian
..............page:17-23
NUMERICAL SIMULATION OF UNSTEADY FLOWS INDUCED BY AN ACCELERATING PROJECTILE
geng ji hui ; xu hou qian
geng ji hui ; xu hou qian
..............page:24-27,34
A STUDY OF TURBULENT FLOW DRAG REDUCTION BY LARGE EDDY BREAK-UP DEVICES
chen qiang ; tang deng bin ; cao qi peng
chen qiang ; tang deng bin ; cao qi peng
..............page:28-33
MOVING TERRESTRIAL VEHICLE IDENTIFICATION BASED ON SHAPE STATISTICS
zhu ming xia ; zhu ji nan ; nie wei rong
zhu ming xia ; zhu ji nan ; nie wei rong
..............page:34-37,46
THE ANALYSIS OF AERODYNAMIC CHARACTER ON GLIDE BULLET TO INCREASE RANGE
wu pin ; zhao run xiang ; tan jun jie ; guo xi fu
wu pin ; zhao run xiang ; tan jun jie ; guo xi fu
..............page:38-41
APPLICATIONS OF HIGHER-ORDER UPWIND SCHEME FOR VISCOUS FLOW OF PROJECTILES
ju yu tao ; zheng ya ; zhou chang sheng
ju yu tao ; zheng ya ; zhou chang sheng
..............page:42-46
STUDY OF HANDING OVER BETWEEN MIDCOURSE GUIDANCE AND TERMINAL GUIDANCE FOR MULTI-PURPOSE MISSILES
luo xi shuang ; zhang tian qiao
luo xi shuang ; zhang tian qiao
..............page:47-50
RESONANCE UNSTABILITY IN BALLISTICS OF FLEXIBLE BODY
wang liang ming ; wang zhong yuan ; yi wen jun
wang liang ming ; wang zhong yuan ; yi wen jun
..............page:51-54
STABLE PRICIPLE OF PNEUMATIC GYRO-RUDDER AND REUSE OF RETIRED GYROSCOPE
xue xiao zhong ; mi zhi hao ; wei jing biao ; shi li xin ; shen jian ping ; pan yong ping
xue xiao zhong ; mi zhi hao ; wei jing biao ; shi li xin ; shen jian ping ; pan yong ping
..............page:55-58
THE RESEARCH OF LAUNCH DYNAMICS OF CASELESS RIFLE
wang yong juan ; zeng wei sheng
wang yong juan ; zeng wei sheng
..............page:59-63
A METHOD TO STUDY RANDOM FACTOR'S EFFECTIONS ON INITIAL DISTURBANCE OF PROJECTILE
wu hong ; zhao you shou
wu hong ; zhao you shou
..............page:64-68
EFFECT OF ATTACK ANGLE MESSUREMENT ERROR ON EXTRACTING AERODYNAMIC COEFFICIENTS
li yin ; zhang feng
li yin ; zhang feng
..............page:69-72,78
THE INFLUENCE OF LAYER WEIGHTS AND LAYER NUMBERS ON FIRING DATA
wang zhao sheng ; guo xi fu
wang zhao sheng ; guo xi fu
..............page:73-78
STUDY ON PRESSURE STABILITY OF ULTRAHIGH-PRESSURE WATER JET SYSTEM
hou jian ; han yu li ; wu fen xiang
hou jian ; han yu li ; wu fen xiang
..............page:79-81
TRAJECTORY PLANNING OF THE TELEVISION-GUIDED AND AIR-TO-GROUND MISSILE
li yong bin ; huang chang qiang ; hao xiao hui
li yong bin ; huang chang qiang ; hao xiao hui
..............page:82-87
THE ERROR ANALYSIS OF FIT METHOD TO UNDERWATER GUN'S PROJECTILE VELOCITY
shen yong ; wang chang ming ; di chang an ; he yun feng ; chen xiao ming
shen yong ; wang chang ming ; di chang an ; he yun feng ; chen xiao ming
..............page:88-91
STUDY ON IDSS OF MULTIPLE TUBE LAUNCHER ROCKET SYSTEM
pei zuo ; ma da wei
pei zuo ; ma da wei
..............page:92-96