An Investigation of Helicopter Dynamic Coupling Using an Analytical Model
- 1 October 1996
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 41 (4) , 322-330
- https://doi.org/10.4050/jahs.41.322
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage DynamicsJournal of the American Helicopter Society, 1992
- Validation of the Dynamic Response of a Blade‐Element UH‐60 Simulation Model in Hovering FlightJournal of the American Helicopter Society, 1991
- Correlation of Measured Induced Velocities with a Finite‐State Wake ModelJournal of the American Helicopter Society, 1991
- Technical Note: Dynamic Inflow for Practical ApplicationsJournal of the American Helicopter Society, 1988