Experimental Investigation Into the Aerodynamic Characteristics of Airfoils with Triangular and Star Shaped Through Damage-Reference-Cited by-同舟云学术

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Experimental Investigation Into the Aerodynamic Characteristics of Airfoils with Triangular and Star Shaped Through Damage

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Mani Mahmoud¹,Render Peter²

Affiliation:

1. Amirkabir University of Technology

2. Loughborough University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4978

Reference22 articles.

1. A. J. Irwin, "Investigation into Aerodynamic Effects of Simulated battle Damage to a Wing," Ph.D. Dissertation ,Loughborough Univ.,Loughborough,U.K.1998

2. Farley, G.L. " Effects of Low- Velocity or Ballistic Impact Damage on the Strength of Thin Composite and Aluminium Shear Panels,"NASATech.Paper2441,1985.

3. CurryJ.M."CarbonFibreCompositeWingSurvivabilityResearch,"BritishAerospaceReportBae/810/TP/29,1982.

4. NASATMX-1550,1968.

Cited by 3 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. A Slider-Type Trim Strategy to Deal with Wing Perforation Damage Based on CFD;Lecture Notes in Electrical Engineering;2021-11-02

2. Investigation of the flowfield induced by simulated battle damage;The Aeronautical Journal;2017-08-25

3. Analysis of Single Hole Simulated Battle Damage on a Wing Using Particle Image Velocimetry;33rd AIAA Applied Aerodynamics Conference;2015-06-19

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