Accession Number : AD0091235


Title :   EFFECTS OF ROTOR BLADE TORSIONAL FLEXIBILITY IN HOVERING FLIGHT


Descriptive Note : Technical rept.,


Corporate Author : HONEYWELL INC HOPKINS MN


Personal Author(s) : WARSETT, PAUL


Report Date : 31 DEC 1955


Pagination or Media Count : 44


Descriptors :   *HELICOPTERS, *ROTOR BLADES (ROTARY WINGS), CONTROL SYSTEMS, OSCILLATION, STABILITY.


Subject Categories : HELICOPTERS


Distribution Statement : APPROVED FOR PUBLIC RELEASE