Accession Number:

ADA801232

Title:

Tests of the NACA 64 sub 1 A212 Airfoil Section with a Slat, a Double Slotted Flap, and Boundary-Layer Control by Suction

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1947-05-01

Pages:

0057

Identifiers:

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

4.83MB