Accession Number:

AD0657565

Title:

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.

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

Report Date:

1966-06-24

Pagination or Media Count:

374.0

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 VSTOL 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 VSTOL aircraft Low speed aerodynamic problems associated with helicopters and VSTOL aircraft Selected research results and recommendations for aerodynamic research Recommendations for aerodynamic research on helicopters and VSTOL aircraft.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • VSTOL
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE