Accession Number:

AD0630924

Title:

WIND TUNNEL TEST OF 1/7 SCALE MODEL OV-1

Descriptive Note:

Final rept.

Corporate Author:

GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE NY

Personal Author(s):

Report Date:

1965-12-01

Pagination or Media Count:

101.0

Abstract:

Wind tunnel tests were conducted on a 17 scale model of the OV-1 airplane to determine the power-off drag, lift, and pitching moment coefficients of the model and its various components. Significant drag differences were measured between production canopy and nacelle configurations and streamlined fuselage and nacelle configurations, but are not considered applicable. No other significant drag differences were measured.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE