Analysis of the Transonic Flow Around a Unmanned Combat Aerial Vehicle Configuration-Reference-Cited by-同舟云学术

Analysis of the Transonic Flow Around a Unmanned Combat Aerial Vehicle Configuration

Published:2018-03 Issue:2 Volume:55 Page:571-586
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Zimper Dirk¹,Hummel Dietrich²

Affiliation:

1. German Aerospace Center (DLR), Program Coordination Defence and Security Research, 51147 Cologne, Germany

2. Braunschweig University of Technology, 38108 Brunswick, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033697

Reference18 articles.

1. ElsenaarA.HjembergL.BütefischK. A.BanninkW. J. “The International Vortex Flow Experiment, Validation of Computational Fluid Dynamics,” AGARD Rept. AGARD-CP-437, Vol. 1, 1988, pp. 9.1–9.23.

2. Review of the Second International Vortex Flow Experiment (VFE-2)

3. HummelD. “The International Vortex Flow Experiment 2 (VFE-2): Objectives and Overview. In: Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft,” Research and Technology Organization, Task Group AVT-113 Summary Rept. RTO-TR-AVT-113, Neuilly-sur-Seine, France, 2009, Chap. 17.

4. Analysis of Transonic Flow on a Slender Delta Wing Using CFD

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