Programmed Pilotage as a Means of Improving Rotorcraft Performance in Level Flight.

Abstract

Airframe drag reduction and engine duct design, while necessary to the improvement of performance, cannot alone offset the aerodynamic limitations inherent in rotary wing flight. The latter, which have become predominant with the advent of high output turboshaft engines must then be overcome by other means discussed in this paper. Programmed pilotage techniques which utilize real-time flight data to vary aerodynamic parameters are investigated and incorporated in the preliminary design of a high-speed rotorcraft. The rotor speed and the contribution of lift from a fixed wing are thus optimized throughout the flight envelope, thereby greatly enhancing level flight speed characteristics. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0736537

Entities

People

  • Robert Alan Wildman

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Drag
  • Drag Reduction
  • Engines
  • Flight
  • Flight Speeds
  • Helicopter Engines
  • Helicopters
  • Level Flight
  • Rotary Wing Aircraft
  • Turboshaft Engines
  • Vehicles

Readers

  • Aerospace Engineering
  • Systems Analysis and Design