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Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings: user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Paine, A. A. |
| Copyright Year | 1972 |
| Description | The input data required to execute the computer program AIC/INT (aerodynamic influence coefficients with interference) are presented. The purpose of the computer program is to generate aerodynamic forces for a pair of plane and interfering nearly parallel, non-coplanar wings at supersonic Mach numbers. A finite element technique has been employed. Planforms are described by triangular elements and diaphragm regions are generated automatically. |
| File Size | 1181164 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730004563 |
| Archival Resource Key | ark:/13960/t9w13tv1f |
| Language | English |
| Publisher Date | 1972-08-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Finite Element Method Numerical Analysis Wings Aerodynamic Configurations Unsteady Aerodynamics Interference Lift Aerodynamic Forces Aerodynamic Characteristics Interference Drag Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |