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Geometry requirements for unsteady aerodynamics in aeroelastic analysis and design
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Yates Jr., E. C. Morino, L. |
| Copyright Year | 1978 |
| Description | Aircraft geometry requirements for unsteady aerodynamic computations are discussed and differences between requirements for steady and unsteady flow are emphasized within the framework of a general potential-flow aerodynamic formulation. Its implementation in a computer program called SOUSSA (Steady, Oscillatory, and Unsteady Subsonic and Supersonic Aerodynamic is detailed. |
| File Size | 6627933 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780025103 |
| Archival Resource Key | ark:/13960/t9z07xp0r |
| Language | English |
| Publisher Date | 1978-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wing Oscillations Descriptive Geometry Unsteady Aerodynamics Structural Design Criteria Aircraft Design Aeroelasticity Aerodynamic Characteristics Aerodynamic Loads Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |