Accession Number:

ADA801268

Title:

Wind-Tunnel Tests of Ailerons at Various Speeds. 4 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-Chord Extreme Blunt-Nose Balance on the NACA 23012 Airfoil

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1943-08-01

Descriptive Note:

Wartime rept.

Pages:

0048

Identifiers:

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

1.09MB