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