Frequency Domain Flutter Boundary Computations Using Navier-Stokes Equations on Superclusters-Reference-Cited by-同舟云学术

Frequency Domain Flutter Boundary Computations Using Navier-Stokes Equations on Superclusters

Published:2014-09 Issue:5 Volume:51 Page:1640-1642
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Guruswamy Guru P.¹

Affiliation:

1. Fundamental Modeling and Simulation Branch, NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032126

Reference12 articles.

1. Mil’M. L. “Helicopters Calculation and Design-Volume I: Aerodynamics,” NASA TD-F-494, Sept. 1967, pp. 379–380.

2. Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data

3. GuruswamyG. P. “Aeroelastic Stability and Time Response Analysis of Conventional and Supercritical Airfoils in Transonic Flow by the Time Integration Method,” Ph.D. Thesis, Dept. of Aeronautics and Astronautics, Purdue Univ., Lafayette, IN, Dec. 1980, http://docs.lib.purdue.edu/dissertations/AAI8113693 [retrieved 2014].

4. Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2

5. WilcoxK. “Reduced-Order Models for Aeroelastic Control of Turbomachines,” Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, Feb. 2000.

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