Computational Design of a Krueger Flap Targeting Conventional Slat Aerodynamics-Reference-Cited by-同舟云学术

Computational Design of a Krueger Flap Targeting Conventional Slat Aerodynamics

Published:2016-05-27 Issue: Volume: Page:
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Container-title:22nd AIAA/CEAS Aeroacoustics Conference
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Author:

Akaydin H. Dogus¹,Housman Jeffrey A.¹,Kiris Cetin C.¹,Bahr Christopher J.²,Hutcheson Florence V.²

Affiliation:

1. NASA Ames Research Center

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2958

Reference28 articles.

1. 1Rudolph, P. K. C. “High-Lift systems on Commercial Subsonic Airliners,” Contractor Report 4746, NASA, 1996.

2. An experimental investigation of the insect shielding effectiveness of a Krueger flap/wing airfoil configuration

3. 4BoeingCommercialAirplaneGroup,Seattle,Washington,“HighReynoldsNumberHybridLaminarFlowControl(HLFC) Flight Experiment II. Aerodynamic Design,” Contractor Report CR-1999-209324, NASA, 1999.

4. The aerodynamic design of multi-element high-lift systems for transport airplanes

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