Preliminary Study on the Design Principles of Civil Aircraft Production Flight Test Procedure

Author(s):  
Zhixia Yin ◽  
Lafei Le ◽  
Dacheng Tian
Micromachines ◽  
2018 ◽  
Vol 9 (12) ◽  
pp. 630 ◽  
Author(s):  
Yidong Gan ◽  
Hongzhi Zhang ◽  
Branko Šavija ◽  
Erik Schlangen ◽  
Klaas van Breugel

Cement paste is the main binding component in concrete and thus its fundamental properties are of great significance for understanding the fracture behaviour as well as the ageing process of concrete. One major aim of this paper is to characterize the micromechanical properties of cement paste with the aid of a nanoindenter. Besides, this paper also presents a preliminary study on the fatigue behaviour of cement paste at the micrometer level. Miniaturized cantilever beams made of cement paste with different water/cement ratios were statically and cyclically loaded. The micromechanical properties of cement paste were determined based on the measured load-displacement curves. The evolution of fatigue damage was evaluated in terms of the residual displacement, strength, and elastic modulus. The results show that the developed test procedure in this work is able to produce reliable micromechanical properties of cement paste. In addition, little damage was observed in the cantilever beams under the applied stress level of 50% to 70% for 1000 loading cycles. This work may shed some light on studying the fatigue behaviour of concrete in a multiscale manner.


2021 ◽  
Vol 2136 (1) ◽  
pp. 012016
Author(s):  
Jingtao Wu ◽  
Pei Wang ◽  
Jin Cai ◽  
Ying Liu

Abstract In the process of civil aircraft airworthiness, analyzing power quality is the key to verify whether the power supply system meets the requirements of the clause. This paper makes deep research on the domestic and foreign power supply quality standard files and detailed introduces the characteristics of the power supply quality standard files. Then, comparative and analysis give suggestions which tally with power supply quality test requirements. Finally, define the special power supply quality test method for the practical engineering specifically, and power supply quality test characteristic in civil aircraft flight test, to provide guidance help for the future civil aircraft models.


2019 ◽  
Vol 60 (1) ◽  
pp. 129-141
Author(s):  
L. Pesaresi ◽  
A. Fantetti ◽  
F. Cegla ◽  
L. Salles ◽  
C.W. Schwingshackl

Abstract Friction joints are one of the fundamental means used for the assembly of structural components in engineering applications. The structural dynamics of these components becomes nonlinear, due to the nonlinear nature of the forces arising at the contact interface characterised by stick-slip phenomena and separation. Advanced numerical models have been proposed in the last decades which have shown some promising capabilities in capturing these local nonlinearities. However, despite the research efforts in producing more advanced models over the years, a lack of validation experiments made it difficult to have fully validated models. For this reason, experimental techniques which can provide insights into the local dynamics of joints can be of great interest for the refinement of such models and for the optimisation of the joint design and local wear predictions. In this paper, a preliminary study is presented where ultrasound waves are used to characterise the local dynamics of friction contacts by observing changes of the ultrasound reflection/transmission at the friction interface. The experimental technique is applied to a dynamic friction rig, where two steel specimens are rubbed against each other under a harmonic tangential excitation. Initial results show that, with a controlled experimental test procedure, this technique can identify microslip effects at the contact interface.


1965 ◽  
Vol 69 (658) ◽  
pp. 662-679 ◽  
Author(s):  
J. M. Naish

Recent work on the Head-Up Display (HUD) has shown properties of continuous transition, easy learning and accurate use, when certain design principles are followed. Use of HUD in manual landing has suggested application as a monitor for automatic landing and another use is for the directed take-off.Developments in display techniques have led to a proposal for an electronic flight instrument display (EFID), suitable for head-down, as well as head-up presentation. Economy in presentation area may result from compressing a number of displays into a single format, and from using the same area for a number of displays presented in sequence.Similar flexible techniques applied to the topographical map display suggest a general-purpose plan position display, complementing the “front elevation” display of flight instruments. These ideas are combined in a proposal for an advanced cockpit layout.


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