Accession Number:

ADA532304

Title:

Design and Experimental Results for the S407 Airfoil

Descriptive Note:

Final rept. Sep 2007-Jun 2010

Corporate Author:

AIRFOILS INC PORT MATILDA PA

Personal Author(s):

Report Date:

2010-08-01

Pagination or Media Count:

88.0

Abstract:

An 11.43-percent-thick airfoil, the S407, intended for rotorcraft applications has been designed and analyzed theoretically and verified experimentally in The Pennsylvania State University Low-Speed, Low-Turbulence Wind Tunnel. The two primary objectives of high maximum lift and low profile drag have been achieved. The constraints on the pitching moment and the airfoil thickness have been satisfied. The airfoil exhibits a sharp stall, which does not meet the design objective. Comparisons of the theoretical and experimental results generally show good agreement.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE