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'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds

IR@NAL: CSIR-National Aerospace Laboratories, Bangalore

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Title 'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds
 
Creator Ramamoorthy, P
Premageetha, BK
 
Subject Fluid Mechanics and Thermodynamics
 
Description An existing computer software package for the determination of lift, drag and pitching moment of the finite wing is ported onto PS 386/387 system and,validated against known examples. This software is presently designated as AEROWING and is used to obtain the loads on the wing of an RPV (Remotely piloted Vehicle).quot; 13; The results prove that the software can provide a tool for the wing analysis amp; design.
 
Publisher National Aeronautical Laboratory
 
Date 1991-03
 
Type Proj.Doc/Technical Report
NonPeerReviewed
 
Format application/pdf
 
Identifier http://nal-ir.nal.res.in/2942/1/trpd_cf_9101_txt.pdf
Ramamoorthy, P and Premageetha, BK (1991) 'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
 
Relation http://nal-ir.nal.res.in/2942/