NONLINEAR FLAP-LAG DYNAMICS OF HINGELESS HELICOPTER BLADES IN HOVER AND IN FORWARD FLIGHT

被引：13

作者：

FRIEDMANN, P

TONG, P

机构：

[1] UNIV CALIF, SCH ENGN & APPL SCI, MECH & STRUCT DEPT, LOS ANGELES, CA 90024 USA

[2] MIT, DEPT AERONAUT & ASTRONAUT, CAMBRIDGE, MA 02139 USA

来源：

关键词：

D O I：

10.1016/S0022-460X(73)80047-1

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

引用

页码：9 / 31

页数：23

共 18 条

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[12]

MILLER RH, 1956, J AM HELICOPTER SOC, V1, P19

[13]

MINORSKY N, 1962, NONLINEAR OSCILLATIO

[14] A PERTURBATION METHOD FOR TREATING NONLINEAR OSCILLATION PROBLEMS [J].

NAYFEH, AH .

JOURNAL OF MATHEMATICS AND PHYSICS, 1965, 44 (04) :368-&

[15]

Ormiston RA, 1972, J AM HELICOPTER SOC, V17, P2, DOI DOI 10.4050/JAHS.17.2

[16]

TONG P, 1972, 2 ATM FLIGHT MECH C

[17]

YOUNG MI, 1964, J AM HELICOPTER SOC, V8, P12

[18]

YOUNG MI, 1962, 18 ANN FOR AM HEL SO