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Airfoil / Lift / Camber / Drag / Stall / Foil / Angle of attack / Wing / Helicopter / Aerodynamics / Aerospace engineering / Fluid dynamics


The Mesicopter: A Miniature Rotorcraft Concept Phase II Interim Report Ilan Kroo, Fritz Prinz (P.I.’s) Michael Shantz (Lecturer) Peter Kunz, Gary Fay, Shelley Cheng, Tibor Fabian, Chad Partridge (Ph.D. students) Stanfo
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Document Date: 2000-08-01 20:51:15


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City

Tibor Fabian / /

Company

Constant Thickness Airfoils Manufacturing / Re lC / Mead / /

Facility

Stanford University / /

IndustryTerm

manufacturing techniques / direct solution / manufacturing / iterative solution / manufacturing minimum gage / lower manufacturing limit / Power law fitting / e -f / power systems / near-term and longer-term applications / number applications / steady-state solution / /

Organization

NIAC / National Aeronautics and Space Administration / Stanford University / DARPA / /

Person

Chad Partridge / Michael Shantz / Ilan Kroo / Fritz Prinz / Shelley Cheng / Peter Kunz / Gary Fay / /

Position

representative / Lecturer / /

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