Investigation of the maximum spin-up coefficients of friction obtained during tests of a landing gear having a static-load rating of 20,000 pounds / by Sidney A. Batterson.

Saved in:

Bibliographic Details
Main Author:	Batterson, Sidney A.
Corporate Authors:	United States. National Aeronautics and Space Administration, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington [D.C.] : National Aeronautics and Space Administration, [1959]
Series:	NASA memorandum ; 12-20-58L.
Subjects:	Airplanes > Landing gear > Testing. Dead loads (Mechanics) Friction.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.10:12-20-58 L
NAS 1.10:12-20-58 L	Available Place a Hold