Accession Number:

ADB805345

Title:

Pressure-Distribution Investigation of an NACA 0009 Airfoil with an 80-Percent-Chord Plain Flap and Three Tabs

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1940-05-01

Pagination or Media Count:

36.0

Abstract:

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE