A comparison of inviscid flow past airfoils by the full potential and euler codes
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
A comparison of inviscid flow past airfoils by the full potential and euler codes
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| Creator |
Gopinath, R
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| Subject |
Fluid Mechanics and Thermodynamics
Aeronautics (General) |
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| Description |
The inviscid flow past a BGK-1, NACA0012 amp; NACA0006 airfoils at a few subsonc Mach numbers amp; incidence, is computed by twe Full Potential Codes - one developed in this Divsiion which is an improvement over the basic code developed by Le Carlson (NAL SOF 0008) amp; the other. a BGKcode, (NAL SOF 0005) and the Euler code, for the 'free air' case and compared. An assessment of the capabilities of these codes, the computing times amp; hence, their appropriateness for any particular case as defined by the airfoil, Mach number and incidence, is made in this study
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| Publisher |
National Aeronautical Laboratory
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| Date |
1991-11
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| Type |
Proj.Doc/Technical Report
NonPeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/1796/1/tr_pdcf_9028_R85707_txt.pdf
Gopinath, R (1991) A comparison of inviscid flow past airfoils by the full potential and euler codes. Technical Report. National Aeronautical Laboratory, Bangalore, India. |
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| Relation |
http://nal-ir.nal.res.in/1796/
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