Applying the lifting surface method to the blade tip of a hovering helicopter-Reference-Cited by-同舟云学术

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Applying the lifting surface method to the blade tip of a hovering helicopter

Published:1989 Issue:11 Volume:17 Page:1455-1466
ISSN:0898-1221
Container-title:Computers & Mathematics with Applications
language:en
Short-container-title:Computers & Mathematics with Applications

Author:

Isser A.,Rosen A.

Publisher

Elsevier BV

Subject

Computational Mathematics,Computational Theory and Mathematics,Modelling and Simulation

Reference25 articles.

1. Subsonic and transonic potential flow over helicopter rotor blades;Caradonna;AIAA J.,1972

2. Unsteady subsonic and transonic potential flow over helicopter rotor blades;Isom;NASA-CR-2463,1974

3. Analysis of the quasi-steady flow about an isolated lifting helicopter rotor blade;Arieli;JIAA,1979

4. Effect of tip shape on blade loading characteristics and wake geometry for a two-bladed rotor in hover;Ballard;J. Am. Helicopter Soc.,1980

5. Influence of rotor blade tip shape on tip vortex shedding—an unsteady, inviscid analysis;Maskew,1980

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Dynamic Mesh Analyses of Helicopter Rotor–Fuselage Flow Interaction in Forward Flight;Journal of Aerospace Engineering;2016-11

2. Novel Approach to Axisymmetric Actuator Disk Modeling;AIAA Journal;2008-11

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