Usng Periodic Perturbations for Download Alleviation on Tilt-rotor Airplane Models in Hover-Reference-Cited by-同舟云学术

Usng Periodic Perturbations for Download Alleviation on Tilt-rotor Airplane Models in Hover

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:2nd AIAA Flow Control Conference
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Author:

Stalker Aaron¹,Cerchie Dino¹,Cullen Lach¹,Wygnanski Israel¹

Affiliation:

1. University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2515

Reference15 articles.

1. Felker FF, Light JS. Rotor/Wing Aerodynamic Interactions in Hover. NASA Technical Memorandum88255, May1986.

2. Felker FF, Shinoda PR, Heffernan RM & Sheehy HF. Wing Force and Surface Pressure Data from a Hover Test of a 0.658-Scale V-22 Rotor and Wing. NASA Technical Memorandum102244, February1990.

3. The delay of turbulent boundary layer separation by oscillatory active control

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