Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings-Reference-Cited by-同舟云学术

Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings

Published:2018-07 Issue:7 Volume:56 Page:2840-2855
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Brooks Timothy R.¹,Kenway Gaetan K. W.¹,Martins Joaquim R. R. A.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48105

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056603

Reference42 articles.

1. SchmittV.CharpinF. “Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers,” Rept. 138, Office National d’Etudes et Recherches Aerospatiales, Chatillon, France, 1979.

2. Drag prediction of engine-airframe interference effects using unstructured Navier-Stokes calculations

3. Development of a Common Research Model for Applied CFD Validation Studies

4. Investigation of Aeroelastic Effects on the NASA Common Research Model

5. Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark

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