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
      V/STOL
      Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE