Accession Number : AD0691194

Title :   THE INSTRUMENTATION OF THE S-2 AIRCRAFT FOR STABILITY AND CONTROL FLIGHT TESTING.

Descriptive Note : Master's thesis,

Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s) : Duncan,Thomas John

Report Date : APR 1969

Pagination or Media Count : 93

Abstract : A Navy US-2A aircraft was instrumented for use in stability and control flight testing. Various methods of recording and sensing the aerodynamic parameters necessary to evaluate stability and control flight testing were investigated. A magnetic tape recorder, obtained on a loan basis, was calibrated and installed to provide a means of recording airborne data. Using available equipment, sensing devices were installed in the aircraft and calibrated to measure control forces, control surface position and normal acceleration. The completed installation provides the means for sensing and recording those aerodynamic parameters most difficult to measure without electronic aids. It also allows for the incorporation of additional sensing and recording devices should they become available. (Author)

Descriptors :   (*UTILITY AIRCRAFT, FLIGHT TESTING), (*FLIGHT TESTING, INSTRUMENTATION), STABILITY, MAGNETIC RECORDING SYSTEMS, AERODYNAMIC CONTROL SURFACES, DETECTORS, NAVAL AIRCRAFT, ACCELERATION, THESES

Subject Categories : Transport Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE