COMMENT ON THE STABILITY DERIVATIVES OF A WING-BODY-VERTICAL TAIL CONFIGURATION

被引:3
作者
BRYSON, AE
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 01期
关键词
D O I
10.2514/8.2916
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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页码:59 / 59
页数:1
相关论文
共 3 条
[1]   STABILITY DERIVATIVES FOR A SLENDER MISSILE WITH APPLICATION TO A WING-BODY-VERTICAL-TAIL CONFIGURATION [J].
BRYSON, AE .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (05) :297-308
[2]   ON DETERMINING THE ADDITIONAL APPARENT MASS OF A WING-BODY-VERTICAL-TAIL CROSS SECTION [J].
SUMMERS, RG .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (12) :856-857
[3]  
WARD GN, 1949, Q J MATH APPL MECH 1, V2