CANARD DROGUE DEPRESSOR

Abstract

The design and development of an in-flight refueling drogue aerodynamic depression system is described. Results of dynamically similar model and full scale wind tunnel tests, actual flight evaluations, and analytical investigations of the system stability characteristics are discussed. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 14, 1961
Accession Number
AD0263431

Tags

DTIC Thesaurus Topics

  • Depression
  • Refueling
  • Test And Evaluation
  • Test Facilities
  • Test Methods
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Aerospace logistics and air mobility.
  • Marine Hydrodynamics