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Rummer, D. I.

Publications and source records attributed to Rummer, D. I..

Development of a simple, self-contained flight test data acquisition system

The flight test system described combines state-of-the-art microprocessor technology and high accuracy instrumentation with parameter identification technology which minimize data and flight time requirements. The system was designed to avoid permanent modifications of the test airplane and allow quick installation. It is capable of longitudinal and lateral-directional stability and control derivative estimation. Details of this system, calibration and flight test procedures, and the results of the Cessna 172 flight test program are presented. The system proved easy to install, simple to operate, and capable of accurate estimation of stability and control parameters in the Cessna 172 flight tests.

Clarke, R.

Data acquisition/reduction system for flight testing general aviation aircraft

The development of a data acquisition/reduction system for use in the flight testing of general aviation aircraft is described. Design objectives for the system are adequate accuracy, ease of installation and removal from aircraft, simplicity of operation, and low cost. A 16-channel working system has been constructed, and tested in the collection of flight test data from a Cessna 172 aircraft, which uses as the basis of its design an AIM65 microcomputer. Data is reduced with a MINC minicomputer system. Attention is given to the onboard installation of computer, battery and transducer modules incorporated by the system.

Rummer, D. I.

A microcomputer-based system for noise characteristics analysis

A description is given of the design and use of a microcomputer-based system for the analysis and prediction of interior noise levels in general aviation aircraft constructed from novel materials. The system consists of a test chamber divided into two parts by a panel which has been fabricated from the material or combination of materials to be tested. A noise generator applies noise to one side of the specimen, while the microcomputer system measures and records the noise spectra on both sides of the specimen, so that its attenuation properties may be calculated and displayed by both a color CRT and X-Y plotter hard copy.

Mosser, M. A.