Accession Number:

AD0423189

Title:

TRANSONIC AERODYNAMIC TRACK TESTING,

Personal Author(s):

Corporate Author:

NAVAL ORDNANCE TEST STATION CHINA LAKE CALIF

Report Date:

1963-09-01

Abstract:

The design, analysis, and operation of a rocket sled to conduct transonic aerodynamic track tests of a full-scale missile are reported. The sled was designed to use a low-frequency rubber suspension system to isolate track-induced vibrations. This necessitated dynamic stability and six-degree-of-freedom vibration analyses. A three-axle sled allowed the suspension system to remain decoupled despite changes of mass. Onboard instrumentation to record test measurements included high-speed cameras and semiconductor type strain gages. In these tests, controlfin hinge moments and the lift, drag, and centerof-pressure of themissile as functions of speed and angle-of-attack were successfully measured. Author

Pages:

0028

Descriptors:

Communities Of Interest:

File Size:

0.00MB

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