Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage Dynamics
- 1 July 1992
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 37 (3) , 3-17
- https://doi.org/10.4050/jahs.37.3
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- A numerical investigation of blade tip loadings on thick-bladed helicopter rotorsComputers & Mathematics with Applications, 1986
- Iterative Lifting Surface Method for Thick Bladed Hovering Helicopter RotorsJournal of Aircraft, 1981
- Surface Pressure Measurements at the Tip of a Model Helicopter Rotor in HoverJournal of Aircraft, 1978
- The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor PerformanceJournal of the American Helicopter Society, 1972
- A Reassessmemt of Rotor Hovering Performance Prediction MethodsJournal of the American Helicopter Society, 1968
- AN AERODYNAMIC ANALYSIS OF A SINGLEBLADED ROTOR IN HOVERING AND LOW- SPEED FORWARD FLIGHT AS DETERMINED FROM SMOKE STUDIES OF THE VORTICITY DISTRIBUTION IN THE WAKEPublished by Defense Technical Information Center (DTIC) ,1956
- New PublicationsTempo, 1945
- On the vortex theory of screw propellersProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1929