CAL/USAAVLABS SYMPOSIUM PROCEEDINGS. AERODYNAMIC PROBLEMS ASSOCIATED WITH V/STOL AIRCRAFT. VOLUME 4. PANELS ON RECOMMENDED V/STOL AERODYNAMIC RESEARCH, PANEL SUMMARIES, FEATURED SPEAKERS, AND TECHNICAL PAPER DISCUSSIONS. HELD JUNE 22-24, 1966, STATLER-HILTON HOTEL, BUFFALO, NEW YORK.

Abstract

The following technical papers were presented: Aeronautical research requirements as determined from the X-19 and X-100 VTOL programs; Thoughts on progress in rotating-wing aerodynamics; Some possibilities for research on stability and control at STOL flight speeds; Aerodynamic research - improvements of the tilt wing concept; Aerodynamic problem areas of V/STOL aircraft and recommended research; A discussion of low speed VTOL aerodynamic problems and suggestions for related research; Areas of fruitful research and development for rotary wing aircraft; A comeback of low-speed aerodynamics research; Required aerodynamic research for V/STOL aircraft; Low speed aerodynamic problems associated with helicopters and V/STOL aircraft; Selected research results and recommendations for aerodynamic research; Recommendations for aerodynamic research on helicopters and V/STOL aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Jun 24, 1966
Accession Number
AD0657565

Entities

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Engineers
  • Fixed Wing Aircraft
  • Flow Visualization
  • Fluid Dynamics
  • High Lift Devices
  • Hydrodynamics
  • Short Takeoff Aircraft

Readers

  • Academic Conference Management
  • Aerospace Engineering