Aero-Structural Modeling of the Truss-Braced Wing Aircraft Using Potential Method with Correction Methods for Transonic Viscous Flow and Wing-Strut Interference Aerodynamics-Reference-Cited by-同舟云学术

Aero-Structural Modeling of the Truss-Braced Wing Aircraft Using Potential Method with Correction Methods for Transonic Viscous Flow and Wing-Strut Interference Aerodynamics

Published:2019-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aviation 2019 Forum
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Author:

Fugate Jason¹,Nguyen Nhan T.²,Xiong Juntao¹

Affiliation:

1. Stinger Ghaffarian Technologies, Inc.

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. Structural and Aeroelastic Characteristics of Truss-Braced Wings: A Parametric Study

2. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport

3. Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft

4. Bradley, M. K. and Droney, C. K. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA Contractor Report NASA/CR-2011-216847, Boeing Research and Technology, April 2011.

5. Bradley, M. K., Droney, C. K., and Allen, T. J. “Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development,” NASA Contractor Report NASA/CR-2012-217556, Boeing Research and Technology, May 2012.

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