共 24 条
[1]
ANANTHKRISHNAN N, 1994, THESIS INDIAN I TECH
[2]
ANANTHKRISHNAN N, 1994, J AERONAUTICAL SOC I, V46, P25
[4]
CARTMELL M, 1990, INTRO LINEAR PARAMET
[6]
DEVELOPMENT OF AN ANALYTICAL MODEL OF WING ROCK FOR SLENDER DELTA WINGS
[J].
JOURNAL OF AIRCRAFT,
1989, 26 (08)
:737-743
[7]
FURTHER ANALYSIS OF HIGH-RATE ROLLING EXPERIMENTS OF A 65-DEG DELTA-WING
[J].
JOURNAL OF AIRCRAFT,
1994, 31 (06)
:1350-1357