Transition and Drag Measurements on the Boulton Paul Sample of Laminar Flow Wing Construction

Abstract

Contents: Part 1, Measurements in the 13' x 19' Tunnel at the N.P.L. Part 2, Measurements in the No. 2 11.5 ft. Tunnel at the R.A.E. Part 3, Joint Discussion of Results, and Note.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1946
Accession Number
ADA800713

Entities

People

  • J. H. Preston
  • K. W. Kimber
  • N. Gregory

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Boundary Layer
  • Construction
  • Evaporation
  • Films
  • Flow
  • Fluid Mechanics
  • Laminar Flow
  • Leading Edges
  • Low Drag
  • Measurement
  • Pressure Gradients
  • Reynolds Number
  • Thickness
  • Transitions
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Fluid Dynamics.