CAL/USAAVLABS SYMPOSIUM PROCEEDINGS. AERODYNAMIC PROBLEMS ASSOCIATED WITH V/STOL AIRCRAFT. VOLUME II. PROPULSION AND INTERFERENCE AERODYNAMICS. HELD JUNE 23, 1966, STATLER-HILTON HOTEL, BUFFALO, NEW YORK

Abstract

Contents: Predicted and measured performance of two full-scale ducted propellers; Aerothermal dynamic performance of a high bypass tip turbine cruise fan system; Thrust deflection nozzles for VTOL aircraft; Shrouded propeller research at Mississippi State University leading to application on the United States Army XV-11A; The lift, drag and stability of wings immersed in propeller slipstream; Aerodynamic properties of airfoils in nonuniformly sheared flows; Experimental investigation of compound helicopter aerodynamic interference effects; Maximum lift coefficient for STOL aircraft: a critical review.

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Document Details

Document Type
Technical Report
Publication Date
Jun 23, 1966
Accession Number
AD0657563

Entities

People

  • A. R. Kriebel
  • Eugene G. Smith
  • Joe F. Thompson
  • Vincent J. Disabato

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Fixed Wing Aircraft
  • Fluid Dynamics
  • Geometry
  • Pressure Distribution
  • Pressure Measurement
  • Short Takeoff Aircraft
  • Shrouded Propellers
  • Stabilization Systems
  • Test And Evaluation
  • Turbines
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerodynamics/Aeronautics.
  • Aerospace Engineering