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

PDF Url : AD0489862

Report Date : Feb 1966

Pagination or Media Count : 35

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.

Descriptors :   *ROTARY WINGS, *VERTICAL TAKEOFF AIRCRAFT, AUTOGYROS, COMPUTER PROGRAMMING, HELICOPTER ROTORS, HELICOPTERS, MOMENTS, PITCH(MOTION), ROLL, ROTOR BLADES(ROTARY WINGS), WIND TUNNEL MODELS

Subject Categories : Helicopters
      V/STOL
      Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE