An Examination of the Factors Affecting the Thrust Requirements and the Hover and Short Takeoff Performance of Several Jet V/STOL Fighter Concepts,

Abstract

A Study of five jet vertical takeoff and landing fighter concepts was made considering height and attitude control, ground effect, ingestion losses, control bleed effects, installation losses, component weights, and short takeoff performance. A fixed gross weight of 35,000 pounds was assumed for each of the following concepts studied: Lift Plus Lift/Cruise; Lift/Cruise Plus Remote Burner; Lift/Cruise (bleed air for control); Vertical Attitude Takeoff and Landing, and Tilt Wing. Since total mission performance was not included in the study, no conclusion as to the 'best' concept is made, but rather some of the mission/concept tradeoffs are presented. (Author)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1978
Accession Number
ADA058128

Entities

People

  • David W Taylor
  • Richard E. Kuhn

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Fighter Aircraft
  • Flight
  • Fluid Dynamics
  • Fuselages
  • Ground Effect
  • Hot Gases
  • Nose Wheels
  • Propulsion Systems
  • Short Takeoff Aircraft
  • Supersonic Aircraft
  • Vertical Takeoff Aircraft

Readers

  • Aerodynamics/Aeronautics.
  • Naval Engineering and Maritime Security
  • Software Engineering