Accession Number:

AD0874410

Title:

Wind Tunnel Investigation of Airfoils Oscillating in Reverse Flow. Volume 2. Data rept.

Descriptive Note:

Final rept.

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Report Date:

1970-03-01

Pagination or Media Count:

303.0

Abstract:

The report presents the final computer-processed data that resulted from the two-dimensional wind tunnel tests of the Vertol 23010-1.58 airfoil oscillating in reverse flow. A set of tables provides a comprehensive index to more than 250 pages of computer data. This volume also includes a series of C sub N and C sub M versus angle-of-attack and time history data plots, presenting data supplementary to Volume I.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE