NDLI: An investigation of aerodynamic characteristics of wings having vortex flow using different numerical codes

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An investigation of aerodynamic characteristics of wings having vortex flow using different numerical codes

Content Provider	NASA Technical Reports Server (NTRS)
Author	Chaturvedi, S. Ghaffari, F.
Copyright Year	1984
Description	Three different numerical codes are employed to determine the aerodynamic characteristics of wings with separation induced vortex flows. Both flat as well as cambered wings of various planform shapes are studied. The effects of wing thickness, fuselage, notch ratio and multiple vortex modeling on aerodynamic performance of the wing are also examined. The theoretically predicted results are compared with experimental results to validate the various computer codes used in this study. An analytical procedure for designing aerodynamically effective leading edge extension (LEE) for a thick delta wing is also presented.
File Size	10264773
Page Count	31
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840017571
Archival Resource Key	ark:/13960/t8gf5nd0z
Language	English
Publisher Date	1984-04-01
Access Restriction	Open
Subject Keyword	Aerodynamics Performance Prediction Iteration Aircraft Design Aspect Ratio Pitch Inclination Lift Computer Programs Least Squares Method Vortices Delta Wings Mathematical Models Angle of Attack Aerodynamic Characteristics Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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