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Calculation of unsteady transonic aerodynamics for oscillating wings with thickness (computer program)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ruo, S. Y. |
| Copyright Year | 1974 |
| Description | A computer program has been developed to account approximately for the effects of finite wing thickness in the transonic potential flow over an oscillating wing of finite span. The program is based on the original sonic-box program of Rodemich and Andrew, and accounts for the nonuniform flow caused by finite thickness by application of the local linearization concept. A brief description of each subroutine is given, and the method of input is shown in detail. A sample problem as well as a complete listing of the computer program are presented. |
| File Size | 1757620 |
| Page Count | 57 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740025314 |
| Archival Resource Key | ark:/13960/t0dv69p1k |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Numerical Analysis Unsteady Aerodynamics Airfoils Wing Profiles Aerodynamic Characteristics Computer Aided Design Computer Programs Wing Camber Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
