Accession Number:

ADA801202

Title:

Wind-Tunnel Tests of a Piston-Type Control Booster on an Airfoil and Aileron Model

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1943-11-01

Descriptive Note:

Wartime rept.

Pages:

0018

Identifiers:

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

0.75MB