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A computer program for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ramsey, J. A. Cebeci, T. Kaups, K. |
| Copyright Year | 1977 |
| Description | A computer program for calculating three dimensional compressible laminar and turbulent boundary layers on arbitrary wings is described and presented. The computer program consists of three separate programs, namely, a geometry program to represent the wing analytically, a velocity program to compute the external velocity components from a given experimental pressure distribution and a finite difference boundary layer method to solve the governing equations for compressible flows. To illustrate the usage of the computer program, three different test cases are presented and the preparation of the input data as well as the computed output data is discussed in some detail. |
| File Size | 4337567 |
| Page Count | 124 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770017113 |
| Archival Resource Key | ark:/13960/t24b7vx04 |
| Language | English |
| Publisher Date | 1977-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Laminar Boundary Layer Swept Wings Three Dimensional Flow Finite Difference Theory Compressible Boundary Layer Turbulent Boundary Layer Compressible Flow Computer Programs Input/output Routines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
