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):

Report Date:

1955-12-31

Pagination or Media Count:

44.0

Abstract:

Subject Categories:

  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE