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Airfoil / Camber / Ira H. Abbott / Chord / Foil / Differential equation / Derivative / Aerodynamics / Aerospace engineering / NACA airfoil


AIAAALGORITHM FOR CALCULATING COORDINATES OF CAMBERED NACA AIRFOILS AT SPECIFIED CHORD LOCATIONS by Ralph L. Carmichael1
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Document Date: 2009-03-10 18:57:47


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File Size: 84,04 KB

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City

Santa Cruz / /

Company

Public Domain Aeronautical Software / Dover Publications Inc. / Ralph L. Carmichael1 Public Domain Aeronautical Software / Aeronautics and Astronautics Inc. / /

Facility

American Institute of Aeronautics / /

IndustryTerm

domain aeronautical software / present algorithm / /

Organization

National Aeronautics and Space Administration / American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / /

Person

Theodore / Garrick / /

Position

author / General / Aeronautical Engineer / modern designer / /

ProgrammingLanguage

Fortran / /

ProvinceOrState

California / /

Technology

present algorithm / four-step algorithm / 5235 ALGORITHM / CONCLUSIONS An algorithm / /

URL

http /

SocialTag