An Experimental Analysis and Buffet Investigation of the Shockless Lifting Airfoil No. 1 (Analyse Experimentale et Etude du Tremblement du Profil Porteur No. 1 Sans Choc),

Abstract

Results of a second investigation of the shockless lifting airfoil No. 1, performed in the improved NAE high Reynolds number 15 inch x 60 inch two-dimensional test facility, are presented. Better agreement with theoretical design conditions is demonstrated. Off-design characteristics for several Mach numbers are analysed, particularly with regard to maximum lift, buffet and drag divergence. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1973
Accession Number
AD0772727

Entities

People

  • J. J. Kacprzynski

Organizations

  • National Research Council Canada

Tags

DTIC Thesaurus Topics

  • Agreements
  • Buildings And Structures
  • Mach Number
  • Physical Properties
  • Research Facilities
  • Reynolds Number
  • Test Facilities
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.