Development of a Dynamic Wind Tunnel Model for Demonstration of Flow Control Maneuver Effectors-Reference-Cited by-同舟云学术

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Development of a Dynamic Wind Tunnel Model for Demonstration of Flow Control Maneuver Effectors

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:3rd AIAA Flow Control Conference
language:
Short-container-title:

Author:

Pilmoor Matthew¹,Crowther William¹,Wood Norman¹

Affiliation:

1. University of Manchester

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3507

Reference17 articles.

1. Overview of Low Observable Technology and Its Effects on Combat Aircraft Survivability

2. 2M.Gad-el-Hak,FlowControl:Passive,Active,andReactiveFlowManagement,CambridgeUniversityPress,2000.

3. 5B. Gilbert, Directional Control of Large Mass Flows by Fluidics, Flucome 91, ASME 3rd Triennial International SymposiumofFluid Control,Measurement &Visualization,SanFrancisco, CA, US., 1991,pp.283-289.

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2. Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification;Journal of Aircraft;2013-03

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