Accession Number : AD0489862
Title : SUPPLEMENTARY STUDY REPORT ROTOR/WING CONCEPT STUDY,
Corporate Author : HUGHES TOOL CO CULVER CITY CA AIRCRAFT DIV
Personal Author(s) : Head, Robert E.
Report Date : FEB 1966
Pagination or Media Count : 24
Abstract : The basic data and analyses from the Rotor/Wing wind tunnel tests were reported in HTC-AD 65-15 (AD-473 862L, 863L, 864L). Supplementary analyses of the data with respect to Rotor/Wing rolling and pitching moments in the low-rpm range, Rotor/Wing shaft bending moments in 1-g running-rotor flight, horizontal tail efficiency, and Rotor/Wing blade root bending moments are included in this report. (Author)
Descriptors : *ROTARY WINGS), (*VERTICAL TAKEOFF AIRCRAFT, HELICOPTERS, AUTOGYROS, ROLL, PITCH(MOTION), COMPUTER PROGRAMMING, WIND TUNNEL MODELS, HELICOPTER ROTORS, ROTOR BLADES(ROTARY WINGS), MOMENTS.
Subject Categories : Helicopters
Hydraulic and Pneumatic Equipment
Distribution Statement : APPROVED FOR PUBLIC RELEASE