Computer program based on Holzer-Myklestad approach calculates coupled vertical, horizontal, and torsional characteristics of wide variety of hub and blade configurations of practical interest. Program is written in FORTRAN IV.
Natural modes of helicopter rotor blades
NASA Tech Briefs ; 4 , 3
1980-04-01
Miscellaneous
No indication
English
Nondestructive evaluation of helicopter rotor blades using guided Lamb modes
Tema Archive | 2014
|Transonic effects on helicopter rotor blades
TIBKAT | 1981
|Resonant vibration of helicopter rotor blades
TIBKAT | 1954
|Aeroelastic Analysis of Helicopter Rotor Blades
AIAA | 2004
|Performance Optimization of Helicopter Rotor Blades
NTIS | 1991
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