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Aerodynamics / Aeronautics / VTOL aircraft / VTOL / Wing configuration / Wingtip device / Lift-induced drag / V/STOL / Wing loading / Aviation / Aerospace engineering / Aircraft


1 Design and aerodynamic considerations about the civil VTOL aircraft Ray
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Document Date: 2010-12-16 12:25:47


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City

Philadelphia / /

Company

C. Breitsamter N.A. / Ray David Posva Ray Research AG / American Helicopter Society International Inc. / GE / /

Country

United States / /

/

Event

Patent Issuance / /

Facility

University of Stuttgart / Raphael Neuhaus University of Stuttgart / Institute of Aircraft Design / Germany Pierre Wilhelm Swiss Federal Institute of Technology Lausanne / Pénélope Leyland Swiss Federal Institute of Technology Lausanne / Leo P. Hall / /

IndustryTerm

transportation / thrust vectoring device / individual travel requirements / propulsion systems / civil applications / door transportation / extra equipment / /

Organization

Federal Aviation Administration / University of Stuttgart / AOA AR CFD CG MTOW VTOL NOTATION Angle of Attack Aspect Ratio Computational Fluid Dynamics Center of Gravity Maximum Take off Weight Vertical Take off / Institute of Aircraft Design / AR CFD CG MTOW VTOL NOTATION Angle of Attack Aspect Ratio Computational Fluid Dynamics Center of Gravity Maximum Take off Weight Vertical Take off / National Aeronautics and Space Administration / Swiss Federal Institute of Technology Lausanne / NASA CR / /

Person

Jan Roskam / Klaus Kittmann / Woodrow L. Crook / Michael Hirschberg / Harry H. Heyson / Jerry V. Kirk / Brent K. Hodder / /

Position

Contractor / Professor / aircraft forward / /

Product

VTOL / dihedral / /

ProgrammingLanguage

V / /

ProvinceOrState

Pennsylvania / /

Technology

Lift Concept Technology / Fluid Dynamics / simulation / /

URL

http /

SocialTag