Accession Number:

ADA801071

Title:

Tests of a Dynamic Model in NACA Tank No. 1 to Determine the Effect of Length of Afterbody, Angle of Afterbody Keel, Gross Load, and a Pointed Step on Landing and Planing Stability

Personal Author(s):

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1943-03-01

Descriptive Note:

Wartime rept.

Pages:

0030

Identifiers:

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

1.42MB