Jig-Shape Optimization of Low-Boom Supersonic Aircraft-Reference-Cited by-同舟云学术

Jig-Shape Optimization of Low-Boom Supersonic Aircraft

Published:2018-09 Issue:5 Volume:55 Page:2154-2161
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pak Chan-gi¹

Affiliation:

1. NASA Armstrong Flight Research Center, Edwards, California 93523-0273

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034851

Reference19 articles.

1. AEROELASTIC CHALLENGES FOR A HIGH SPEED CIVIL TRANSPORT

2. Conceptual Design of Low-Boom Aircraft with Flight Trim Requirement

3. Sobieszczanski-SobieskiJ.HaftkaR. T. “Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments,” AIAA Paper 1996-0711, Jan. 1996. doi:10.2514/6.1996-711

4. Combined aerodynamic and structural optimization of a high-speed civil transport wing

5. CarlsonH. W.ChuJ.OzoroskiL. P.McCullersL. A. “Guide to AERO2S and WINGDES Computer Codes for Prediction and Minimization of Drag Due to Lift,” NASA TP-3637, 1997.

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Linear and Geometrically Nonlinear Structural Shape Sensing from Strain Data;AIAA Journal;2023-02

2. Flexibility Assessment of the Aeroelastic-flight-dynamic Behavior for Supersonic Aircraft;AIAA SCITECH 2023 Forum;2023-01-19

3. Unsteady Vortex Lattice Linearization and Sensitivity Analyses for Control Models in Supersonic Aircraft Design;AIAA SCITECH 2023 Forum;2023-01-19

4. Linear and Geometrically Nonlinear Structural Shape Sensing from Strain Data using the Basis Function Method;AIAA SCITECH 2023 Forum;2023-01-19

5. Parametric Analysis of Design Characteristics of Supersonic Passenger Aircraft;Recent Developments in High-Speed Transport;2023