EVALUATION OF THE INERTIA COEFFICIENTS OF THE CROSS SECTION OF A SLENDER BODY

被引:7
作者
BRYSON, AE
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1954年 / 21卷 / 06期
关键词
D O I
10.2514/8.3063
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
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页码:424 / 427
页数:4
相关论文
共 9 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]   COMMENT ON THE STABILITY DERIVATIVES OF A WING-BODY-VERTICAL TAIL CONFIGURATION [J].
BRYSON, AE .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (01) :59-59
[3]  
COPSON ET, 1935, THEORY FUNCTIONS COM, P247
[4]   A LIMITING CASE FOR MISSILE ROLLING MOMENTS [J].
GRAHAM, EW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (09) :624-628
[5]  
LAMB H, HYDRODYNAMICS, pCH6
[6]   ON INTERFERENCE FACTORS FOR FINNED BODIES [J].
MILES, JW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (04) :287-287
[7]  
MILNETHOMPSON LM, THEORETICAL HYDRODYN, pCH9
[8]   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
[9]  
WARD GN, 1949, Q J APP MATH MECH 1, V2