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The Prototype Data and the Need for Reinforcement Airliner door is composed of double aluminum, materials LY12CZ, elastic modulus 71GPa, ultimate strength 414MPa, yield strength 270MPa, elongation 15%, stress-strain curves are shown in Figure 1.
Setting-up of reinforced pieces is difficult to avoid the further reduction of the installation space for explosion-combustion power equipments, but it can not cause the unacceptable impact on the main functional dimension of explosion-combustion power equipments.

The data sets for which it was not possible to obtain required similarity between model (after parameters fitting) and DIC measurements were omitted.
Obtained results showed the necessity of the improvement of casting process in terms of the reduction of the residual porosity.

The following conventions were used for data reduction.

The four sets of data (6mm, 8mm, 12mm and 16mm) are designed to simulate and analyze.
The outer surface of the equivalent strain decreases with the increase of the single radial pressure amount reduction.

In order to eliminate disturbance of initial load step, data from 0.01sec to 0.05sec is chosen to analyze.
It’s clear that large fillet leads to a reduction of speed fluctuation which is helpful to obtain a smooth rotation movement of gears.

With reduction of the size of nanostructures below 100 nm, the control of their shape becomes more difficult due to the limit of lithography resolution.
The best agreement between experimental and calculated data was observed in the case of exponential approximation , where a, b and c are the fitting coefficients.

In electrical engineering, rapid prototyping is used due to the continuous reduction in the size of components, which are very complicated to manufacture.
Finally, it has the advantage of very fast data retrieval for preparation and production.

Introduction Gas-liquid separation mechanisms for on-orbit resupply and manned spacecraft have traditionally presented major problems in ground test and flight applications[1].Reduction in the magnitude of the gravity vector will have a profound effect not only on the gas-liquid flow behavior, but also on the technologies that will be required for future space-based platforms[2].
[2] Mcquilen John, Motil Brian, Reduced gravity gas and liquid flows: simple data for complex problems, R.

Fluoride metallurgy, as a complex of technological processes of preparation, cleaning and reduction of fluorides to metals, has been applied primarily in the nuclear industry [3].
From the figure, it is seen that: - at temperature 60 °C ions with mass equal to 19, the hydrogen fluoride are recorded, the lowest intensity of the mass spectrum indicates a slight evolution of hydrogen fluoride from the sample, on the spectrum of X-ray phase analysis the mixture of starting substances is observed; - in the temperature range of 100 °C, the typical mass spectrum of water with insignificant impurities of hydrogen fluoride is observed, the composition according to data of X-ray phase analysis is not changed; - in the temperature range of 135 °C the emission of ammonia is observed that in agreement with the known mechanism of melting of ammonium fluoride with decomposition and the formation of ammonium bifluoride with the evolution of ammonia and the formation of the eutectic mixture NH4F/(NH4F×HF) [5], on the spectrum of X-ray phase analysis the reflexes of ammonium fluoride disappeared that indicates on its melting; - at higher temperature (210 °C) the ammonia continues

Mathematical model of quadrotor UAV Yang [4] proposed the transfer function of roll channel for quadrotor UAV as follows: (1) The rotor system involves controller, elctric motor, reduction box, rotor, and speed sensor.
The crossover operation mixes the binary number by swapping a portion of the data structure