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Finite-difference computations of rotor loads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tung, C. Caradonna, F. X. |
| Copyright Year | 1985 |
| Description | The current and future potential of finite difference methods for solving real rotor problems which now rely largely on empiricism are demonstrated. The demonstration consists of a simple means of combining existing finite-difference, integral, and comprehensive loads codes to predict real transonic rotor flows. These computations are performed for hover and high-advanced-ratio flight. Comparisons are made with experimental pressure data. |
| File Size | 1165245 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850018358 |
| Archival Resource Key | ark:/13960/t4fn62519 |
| Language | English |
| Publisher Date | 1985-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Value Problems Transonic Flow Helicopters Finite Difference Theory Performance Prediction Problem Solving Rotor Aerodynamics Pressure Measurement Equations of Motion Hovering Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |