TL;DR: An affordable technique is proposed for fast quantitative analysis of aerobatics and other complex flight domains of highly maneuverable aircraft, using a generalized autonomous situational model of the "pilot (automaton) – vehicle – operational environment" system as a “virtual test article”.
TL;DR: In this paper, the authors present a research project that has the goal of reducing installation errors in heavy aircraft maintenance, with two large carriers and a large repair station, with the goal to reduce selected error categories.
Abstract: An original instrument for fuel consumption measurement in reciprocating intenal combustion spark ignition engines for light aircraft and motorgliders has been developed and built. It is based on the detection of two parameters. the engine rotational speed and the manifold pressure. The aim of the instrument is to provide a "fuel consumption index" which can be utilized both in "Economy Air Race" competitions and during cruising flight. The instrument is not intended to replace the usual onboard fuel level gauge, but could be used to integrate the flight information with the instantaneous fuel consumption or even with the cruising range indications. Some results of fuel consumption measurements, from both computer simulation and experimental tests, are first presented and then discussed. These were obtained with the instrument installed on the engine during bench tests. Some flight tests were then carried out with the instrument installed on a light aircraft in order to evaluate the instrument response under real operating conditions. The first results thus obtained encourage further development of the instrument.
TL;DR: In this article, a computer model was developed using MADYMO to evaluate the effect of cushion stiffness, belt anchor spacing, and initial belt tension on the performance of automotive child restraint devices.