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:

1955-12-31

Pagination or Media Count:

44.0

Abstract:

Descriptors:

• *HELICOPTERS
• *ROTOR BLADES (ROTARY WINGS)
• CONTROL SYSTEMS
• OSCILLATION
• STABILITY

Subject Categories:

• Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE