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Boundary condition program for aerodynamic lifting surface theory. [using fortran 4
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ray, K. S. Medan, R. T. |
| Copyright Year | 1973 |
| Description | Users manual for a U.S.A. FORTRAN 4 computer program which determines boundary conditions for a thin wing lifting surface program is described. This program, the geometry program, and several other programs are used together in the analysis of lifting, thin wings in steady, subsonic flow according to a kernel function lifting surface theory. The program calculates specific types of boundary conditions automatically such as those necessary to determine pitch and roll damping derivatives. The program also accepts descriptions of the camber or downwash and twist in the form of tables and/or coefficients of equations. The program performs interpolations so that tables and/or coefficients can apply at stations selected by the user and not at stations dictated by the control point locations. |
| File Size | 1451270 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740008586 |
| Archival Resource Key | ark:/13960/t09w56w6g |
| Language | English |
| Publisher Date | 1973-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Conditions Lifting Bodies Aerodynamic Characteristics User Manuals Computer Programs Boundary Layers Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
