Influence of Transonic Flutter on the Conceptual Design of Next-Generation Transport Aircraft-Reference-Cited by-同舟云学术

Influence of Transonic Flutter on the Conceptual Design of Next-Generation Transport Aircraft

Published:2019-05 Issue:5 Volume:57 Page:1973-1987
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Opgenoord Max M. J.¹,Drela Mark¹,Willcox Karen E.²

Affiliation:

1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

2. University of Texas at Austin, Austin, Texas 78712

Funder

SUTD-MIT International Design Center

NASA LEARN

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057302

Reference47 articles.

1. BradleyM. K.DroneyC. K. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA CR-2011-216847, April 2011.

2. Development of the D8 Transport Configuration

3. Review of unsteady transonic aerodynamics: Theory and applications

4. DoggettR. V. Jr.MorganH. G.RaineyA. “An Experimental Investigation of Aerodynamic Effects of Airfoil Thickness on Transonic Flutter Characteristics,” NASA TM X-79, Nov. 1959.

5. COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICS

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