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Space technology / Stall / Wind tunnel / Sideslip angle / Tire / Pitching moment / Slip / Angle of attack / Tundra tire / Aerodynamics / Aerospace engineering / Fluid dynamics


DOT/FAA/AR-xx/xx Office of Aviation Research Washington, D.C[removed]Aerodynamic Effects of Oversized Tires and Modified
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Document Date: 2006-05-23 09:52:43


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City

Washington / DC / Springfield / /

Company

G.G. Thumann S.A. / /

Country

United States / /

Facility

Aviation Research Wichita State University / Water tunnel / Wichita State University / Miller G.G. Thumann S.A. Sanborn D.R. Ellis National Institute / This tunnel / National Institute / /

NaturalFeature

Sting Mount / /

Organization

Normal Force / Federal Aviation Administration / Side Force / National Technical Information Service / Wichita State University / office of Aviation Research Washington / D.C. / LIST OF FIGURES Figure Page 1A Water Tunnel Model Assembly / U.S. Department of Transportation / National Institute / Gear Assembly / Including Gear Assembly / U.S. Department of Transportation Federal Aviation Administration office of Aviation Research Washington / NOMENCLATURE Center of Gravity Wing Span Wing Reference Chord Wing Reference Area Freestream Dynamic Pressure Freestream Flow Density Freestream Flow Speed Reynolds Number Freestream Flow Viscosity Angle of Attack / United States Government / Work Unit / Small Utility Airplane L.S. Miller G.G. Thumann S.A. Sanborn D.R. Ellis National Institute for Aviation Research Wichita State University Wichita / /

Person

Piper Super Cub / /

Position

model / EXECUTIVE / CONTENTS EXECUTIVE / model / and C-strut together / /

ProvinceOrState

Kansas / Virginia / Alaska / /

Technology

Alpha / CRM / /

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