X-31 Vector Aircraft, Low Speed Stability & Control, Comparisons of Wind Tunnel Data & Theory (Focus on Linear & Panel Codes)-Reference-Cited by-同舟云学术

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X-31 Vector Aircraft, Low Speed Stability & Control, Comparisons of Wind Tunnel Data & Theory (Focus on Linear & Panel Codes)

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
language:
Short-container-title:

Author:

Nangia Raj¹

Affiliation:

1. Nangia Aero Research

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3898

Reference10 articles.

1. Presented at RTO - AVTSymposium, Loen, Norway, May2001.

2. NANGIA, R.K. "Semi-Empirical Prediction of the Vortex Formation on the VFE-2 Configuration (65 deg. Delta

3. Wings with different LeadingEdgeshapes)", Chapter 33, RTO-AVT-113 Report, Formal Publication 2008.

Cited by 4 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. Engineering Methods Applied to an Unmanned Combat Air Vehicle Configuration;Journal of Aircraft;2012-11

2. CFD analysis of the flow around the X-31 aircraft at high angle of attack;Aerospace Science and Technology;2012-07

3. Comparing and benchmarking engineering methods for the prediction of X-31 aerodynamics;Aerospace Science and Technology;2012-07

4. CFD Analysis of the Flow Around the X-31 Aircraft at High Angle of Attack;27th AIAA Applied Aerodynamics Conference;2009-06-14

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