A Steady Aeroelastic Analysis of an Unmanned Combat Aircraft Vehicle Conceptual Design-Reference-Cited by-同舟云学术

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A Steady Aeroelastic Analysis of an Unmanned Combat Aircraft Vehicle Conceptual Design

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Voss Guido¹,Cumnuantip Sunpeth¹,Neumann Jens¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3020

Reference4 articles.

1. [1]A.Schuette etal,Numerical and Experimentalanalysesof thevorticalflow around theSACCON configuration,28thAIAAAppliedAerodynamicsConference,Chicago,USA,2010

2. [2]M.Galle, Ein Verfahrenzurnumerischen Simulationkompressibler,reibungsbehafteter Stroemungen auf hybridenNetzen,Diss.,DLR-FB99-04,1999

3. [5]J.Neumann,PyCSM-PythonComputationalFluidDynamics andComputationalStructure Machanics Coupling System,SoftwareDocumentation andTechnicalReport,Institute ofAeroelasticity, State: November 2010,Goettingen

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1. Technology challenges of stealth unmanned combat aerial vehicles;The Aeronautical Journal;2017-06-23

2. Development of a wind tunnel experiment for vortex dominated flow at a pitching Lambda wing;CEAS Aeronautical Journal;2014-07-19

3. Vortical flow prediction for the design of a wind tunnel experiment with a pitching lambda wing;CEAS Aeronautical Journal;2014-07-11

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