NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Numerical solution of the Navier-Stokes equations for arbitrary two-dimensional airfoilsA method for numerical solution of the Navier-Stokes equations for the flow about arbitrary airfoils or other bodies is presented. This method utilizes a numerically generated curvilinear coordinate system having a coordinate line coincident with the body contour. Streamlines, velocity profiles, and pressure and force coefficients for several airfoils and an arbitrary rock are given. Potential flow solutions are also presented. The procedure capable of treating multiple-element airfoils, and potential flow results are presented.
Document ID
19760002935
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thames, F. C. (Mississippi State Univ. Mississippi State, MS, United States)
Thompson, J. F. (Mississippi State Univ. Mississippi State, MS, United States)
Mastin, C. W. (Mississippi State Univ. Mississippi State, MS, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Langley Res. Center Aerodynamic Analyses Requiring Advanced Computers, Pt. 1
Subject Category
Aerodynamics
Accession Number
76N10023
Funding Number(s)
CONTRACT_GRANT: NGR-25-001-055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760002919Collected WorksAerodynamic Analyses Requiring Advanced Computers, Part 119760002919Collected WorksAerodynamic Analyses Requiring Advanced Computers, Part 1
No Preview Available