CORRELATION OF WIND-TUNNEL MEASUREMENTS ON THE BASIS OF BLOWING MOMENTUM REQUIRED TO PRODUCE THEORETICAL FLAP EFFECTIVENESS ON AIRPLANE MODELS EQUIPPED WITH BOUNDARY-LAYER-CONTROL DEVICES

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1955
Accession Number
AD0086505

Entities

People

  • E.l. Harkleroad
  • H.r. Chaplin
  • S.t. De Los Santos

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Fixed Wing Aircraft
  • Layers
  • Measurement
  • Momentum
  • Wind Tunnels