TWO-DIMENSIONAL CIRCULATION CONTROL TESTS ON AN NACA 23015 AIRFOIL EQUIPPED WITH A SEALED AND SLOTTED FLAP TO DETERMINE JET MOMENTUM LOSS OVER THE FLAP

Document Details

Document Type
Technical Report
Publication Date
May 01, 1958
Accession Number
AD0215408

Entities

People

  • D.l. Cruse
  • P.e. Morris

Organizations

  • Wichita State University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airfoils
  • Airframes
  • Airplanes
  • Cooperation
  • Fixed Wing Aircraft
  • Momentum
  • Physical Properties
  • Slotted Flaps
  • Two Dimensional
  • Vehicles