Passive shock wave/boundary layer control of a helicopter rotor airfoil in a contoured transonic wind tunnel-Reference-Cited by-同舟云学术

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Passive shock wave/boundary layer control of a helicopter rotor airfoil in a contoured transonic wind tunnel

Published:1987-03-24 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

NAGAMATSU HENRY¹

Affiliation:

1. Rensselaer Polytechnic Institute, Troy, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-438

Reference33 articles.

1. Hilton, W.F., Hi.S.d-Aerodynnmice, Lnngman, Green 11 Co., New York, 1951, PP. 369-383.

Cited by 6 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. Active Control of Normal Shock Wave/Tubulent Boundary Layer Interaction Using "Smart" Piezoelectric Flap Actuators;2nd AIAA Flow Control Conference;2004-06-20

2. Skin Friction Measurements for Recirculating Normal Shock/Boundary-Layer Interaction Control;AIAA Journal;2004-04

3. Simulations of Normal Shock-Wave/Boundary-Layer Interaction Control Using Mesoflaps;Journal of Propulsion and Power;2004-03

4. Skin friction measurements in normal shock wave/turbulent boundary-layer interaction control with aeroelastic mesoflaps;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

5. Theoretical study of passive drag-reduction on transonic airfoils;16th Atmospheric Flight Mechanics Conference;1989-08-14

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