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| Theodorsen Flutter× | Specifik överskotts-effekt× | |
|---|---|---|
| Ämnesområde | Flyg- och rymdteknik | Flyg- och rymdteknik |
| Familj | Process / pipeline | Process / pipeline |
| Ursprungsår≠ | 1935 | 1970s |
| Upphovsperson≠ | Theodore Theodorsen | John Boyd, U.S. Air Force |
| Typ≠ | Stability analysis | Tactical metric |
| Ursprungskälla≠ | Theodorsen, T. (1935). General theory of aerodynamic instability and the mechanism of flutter. NACA Report No. 496. link ↗ | Boyd, J. R., & Hammond, J. A. (1971). The mechanics of air combat. Fighter Weapons Newsletter, US Air Force Tactical Air Command. link ↗ |
| Alias | flutter analysis, aeroelastic stability, Theodorsen's function | Ps, energy maneuverability theory, specific power |
| Närliggande | 3 | 3 |
| Sammanfattning≠ | Theodorsen flutter analysis is a classical aeroelastic method for predicting the onset of flutter, a self-excited oscillation where aerodynamic forces interact with elastic structural motion to cause rapid growth of oscillations. Developed by Theodore Theodorsen in 1935, the method uses frequency-domain analysis with Theodorsen's function to compute aerodynamic forces on oscillating wings. Flutter speed prediction is essential for aircraft certification and structural design. | Specific excess power (Ps) is a metric that quantifies the rate of change of energy per unit weight, representing how quickly an aircraft can trade speed for altitude (or vice versa) at a given flight condition. Developed by John Boyd in the 1970s as part of energy maneuverability theory, Ps is essential for assessing aircraft performance during combat maneuvering, climb, and acceleration. Specific excess power is widely used in military aircraft design, flight envelope analysis, and tactical air combat assessment. |
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