Accession Number:

ADB805295

Title:

Force and Moment Coefficients for a Thin Airfoil with Flap and Tab in a Form Useful for Stability and Control Calculations

Descriptive Note:

Technical note

Corporate Author:

CURTISS-WRIGHT CORP COLUMBUS OH

Personal Author(s):

Report Date:

1945-01-01

Pagination or Media Count:

42.0

Abstract:

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE