Accession Number:

ADA801236

Title:

High-Speed Wind-Tunnel Tests of an NACA 16-009 Airfoil Having a 32.9-Percent-Chord Flap with an Overhang 20.7 Percent of the Flap Chord

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1947-08-01

Descriptive Note:

Technical note

Pages:

0040

Identifiers:

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

3.78MB