Accession Number:

AD0684324

Title:

WIND TUNNEL TESTS OF THIN AIRFOILS OSCILLATING NEAR STALL. VOLUME II. DATA REPORT

Descriptive Note:

Final rept. 27 Jun 1967-15 Aug 1968

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Personal Author(s):

Report Date:

1969-01-01

Pagination or Media Count:

280.0

Abstract:

The report presents the actual computer data that resulted from the two-dimensional tests of thin airfoils oscillating near stall. An introduction provides a general background, and a set of tables forms an index to specific data. More than 200 pages of computer data are included.

Subject Categories:

  • Aerodynamics
  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE