Forward flight analysis of slatted rotors using Navier-Stokes methods-Reference-Cited by-同舟云学术

Forward flight analysis of slatted rotors using Navier-Stokes methods

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Bangalore A.¹,Sankar L.¹

Affiliation:

1. Georgia Inst. of Technology, Atlanta

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-675

Reference45 articles.

1. Noonan, K.W. and Bingham, B.J. "Aerodynamic Characteristics of Three Helicopter Rotor Airfoil Sections from Model Scale to Full Scale at Mach Numbers from 0.35to 0.9," NASA Technical Paper 1701,AVRADCOMTR-80-B-5,1980.

2. Noonan, K. W. and Bingham, B. J. " Two dimensional Aerodynamic Characteristics of Several Rotorcraft Airfoils at Mach Numbersfrom 0.35 to 0.9, "NASATM-X-73990,1977.

3. McAlister, K.W.,Pucci, S.L.,McCroskey,WJ. and Carr,L.W."An Experimental study of Dynamic Stall on AdvancedAirfoil Sections,Volume 2: Pressureand ForceData,"NASATM84245,September 1982.

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