OSCILLATORY PRESSURES IN AN IDEALIZED BOUNDARY LAYER WITH APPLICATION TO CYLINDER FLUTTER

被引：4

作者：

ANDERSON, WJ

机构：

来源：

关键词：

D O I：

10.2514/3.3559

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：865 / &

共 16 条

[1]

ANDERSON WJ, 1962, SM6249 CAL I TECHN G

[2]

ANDERSON WJ, 1965, 65203 AER RES LAB WR

[3]

ANDERSON WJ, 1965, P AIAA S STRUCTURAL

[4]

ANDERSON WJ, 1963, THESIS CALIFORNIA I

[5] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J].

ASHLEY, H ;

ZARTARIAN, G .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12) :1109-1118

[6]

BATDORF SB, 1947, NACA874 LANGL RES CE

[7]

CZARNECKI KR, 1961, TND835 NASA LANGL RE

[8] ON SOME SPECIAL PROBLEMS IN LINEARIZED AXIALLY SYMMETRIC FLOW [J].

DESCLERS, B ;

CHANG, CC .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (02) :127-138

[9]

DONNELL LH, 1934, NACA479 REP, P95

[10] SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCH [J].

FUNG, YC .