TO QUESTION ABOUT SELECTION OF THE OPTIMUM THRUST-WEIGHT RATIO OF VTOL WITH RESPECT TO LIFT ENGINES (K VOPROSU O VYBORE OPTIMALNOI TYAGOVOORUZHENNOSTI AVVP PO PODEMNYM DVIGATELYAM),

Abstract

An analysis is made of the problem of selecting the optimal thrust-weight ratio of lifting engines for vertical takeoff and landing aircraft, taking into account tactical, technical, and economic requirements. The article gives the results of computer calculations of transportation of cost and transport effectiveness as a function of the thrust-weight ratio of the lifting engine. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 12, 1967
Accession Number
AD0674680

Entities

People

  • O. K. Bogdanov
  • V. I. Rudomanov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Computers
  • Marine Transportation
  • Rotary Wing Aircraft
  • Surface Transportation
  • Tilt Rotor Aircraft
  • Transport Ships
  • Transportation
  • Vehicles
  • Vertical Takeoff Aircraft

Readers

  • Aerodynamics/Aeronautics.
  • Information Retrieval
  • Life Cycle Cost Analysis