AN EVALUATION OF THE WING-IN-GROUND EFFECT (WIG) TRANSPORT AIRCRAFT CONCEPT.

Abstract

An evaluation was made of the 'wing in ground effect' (WIG) interface vehicle as a cargo transport. The WIG aircraft designs, with high lift/drag ratios, showed significant increases in payload-range over current and proposed cargo aircraft (specifically, the c-141 and the C-5A). However,results indicate that the C-5A cargo aircraft would have a somewhat higher productivity than the WIG cargo transport. The large differences in cruise speed between these aircraft negated the excellent payload-range capabilities of the WIG aircraft concept. The unique qualities of the WIG may be more effectively utilized in other specialized military aircraft applications.

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0379260

Entities

People

  • Gary W. Brasseur
  • Paul Comisarow

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Design
  • Aircrafts
  • Cargo Aircraft
  • Freight Transportation
  • Ground Effect
  • High Lift
  • Military Aircraft
  • Surface Effect Vehicles
  • Test And Evaluation
  • Transport Aircraft
  • Transport Ships
  • Vehicles

Readers

  • Aerospace Engineering
  • Naval Architecture and Marine Engineering.
  • Systems Analysis and Design