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Aviation / Slip / Dihedral / Stall / Rudder / P-factor / Flight dynamics / Fixed-wing aircraft / Aileron / Aerospace engineering / Aerodynamics / Fluid dynamics


Control and Performance During Asymmetrical Powered Flight Detailed theoretical paper
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Document Date: 2013-08-15 06:18:00


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File Size: 2,13 MB

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Company

AvioConsult / /

Country

United States / /

Facility

Edwards Air Force Base / University of North Dakota In / University of Kansas / University of North Dakota / /

IndustryTerm

required bank angle / banking / bank indicator / bank angle / degree favorable bank angle / bank angle analysis / /

Organization

Empire Test Pilots' School / University of North Dakota In / University of Kansas / Royal Netherlands Air Force / USAF Test Pilot School / IMC / University of North Dakota / European Union / /

Person

Part / Harry Horlings Lt-Col / /

Position

author / tail design engineer for sizing the vertical tail / pilot / Asymmetrical Powered Flight The author / graduate Flight Test Engineer / Consultant / tail design engineer / engineer / founder / /

Product

Dakota / swept wing / dihedral / /

ProvinceOrState

Kansas / North Dakota / California / /

URL

www.avioconsult.com / /

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