Unsteady transonic flow simulation on a full-span-wing-body configuration
Author:
Affiliation:
1. Sterling Federal Systems, Inc., Palo Alto, California
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10063
Reference16 articles.
1. Computational transonic flow about realistic aircraft configurations
2. Transonic Navier-Stokes solutions for a fighter-like configuration
3. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon
4. Unsteady transonics of a wing with tip store
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1. Analysis of the Transonic Flutter of Supersonic Transport Wings;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02
2. Computational Transonic Flutter Solutions for Cranked Wing Planforms;55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2014-01-10
3. Transonic flow potential method development at Ames research center;Computers & Fluids;2009-03
4. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01
5. Higher approximations of the transonic expansion in problems of unsteady transonic flow;Journal of Applied Mathematics and Mechanics;1997-01
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