Further analysis of high-rate rolling experiments of a 65 deg delta wing-Reference-Cited by-同舟云学术

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Further analysis of high-rate rolling experiments of a 65 deg delta wing

Published:1993-01-11 Issue: Volume: Page:
ISSN:
Container-title:31st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

ERICSSON LARS¹,HANFF ERNEST¹

Affiliation:

1. National Research Council of Canada, Inst. for Aerospace Research, Ottawa

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-620

Reference20 articles.

1. IIanff,E. S.andJenkins,S.B. "Large-Amplitude High-RateRoll Experiments on a Deltaand Double DeltaWing",AIM Paper 90-0223,Jan. 1990.

2. Ericsson,L. E. "AnalysisofWind-Tunnel Data Obtainedin High-RateRolling Experiments with SlenderDeltaWings",LAR Contractor Report IAR-CR-14,August 1991.

3. Fluid dynamics of unsteady separated flow. Part I. Bodies of revolution

Cited by 12 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. Quantitative Imaging in Proper Orthogonal Decomposition of Flow Past a Delta Wing;AIAA Journal;1998-07

2. Instantaneous Crossflow Topology on a Delta Wing in Presence of Vortex Breakdown;Journal of Aircraft;1998-03

3. Effects of leading-edge sweep angle on nonzero trimmed roll angles;Journal of Aircraft;1996-07

4. Critical states and flow structure on a 65-deg delta wing;Journal of Aircraft;1996-03

5. Fluid/motion coupling in conceptual supermaneuvers;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

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