What was learned from the new VFE-2 experiments-Reference-Cited by-同舟云学术

What was learned from the new VFE-2 experiments

Published:2013-01 Issue:1 Volume:24 Page:77-88
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Luckring James M.,Hummel Dietrich

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. J. Chu, J.M. Luckring, Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges, NASA TM 4645, 1996.

2. F. Coton, S. Mat, R. Galbraith, Low speed wind tunnel characterization of the VFE-2 wing, AIAA Paper 2008-0382, 2007.

3. W. Fritz, Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge, AIAA Paper 2008-0393, 2008.

4. A. Furman, Ch. Breitsamter, Investigations of flow phenomena on generic delta wing, in: ICAS Proceedings Hamburg 2006, Paper 3.1.2, 2006.

5. A. Furman, Ch. Breitsamter, Stereo-PIV and hot-wire investigations on delta wing with sharp and rounded leading edge, in: 1st CEAS Conference Berlin 2007, Paper 2007-430, 2007.

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