Accession Number:

ADA801101

Title:

Spin-Tunnel Tests of Airplane Models with Extreme Variations in Mass Distribution along the Three Body Axes

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1945-03-01

Descriptive Note:

Wartime rept.

Pages:

0035

Identifiers:

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

0.79MB