scholarly journals On-board compressor water injection for civil aircraft emission reductions: Range performance with fuel burn analysis

2019 ◽  
Vol 67 ◽  
pp. 449-463
Author(s):  
David Alejandro Block Novelo ◽  
Uyioghosa Igie ◽  
Devaiah Nalianda
2015 ◽  
Vol 19 (4) ◽  
pp. 278-287 ◽  
Author(s):  
Hee-jin Joo ◽  
Ho-yon Hwang ◽  
Byung-woon Park ◽  
Dongwook Lim
Keyword(s):  

2006 ◽  
Vol 110 (1110) ◽  
pp. 495-510 ◽  
Author(s):  
R. K. Nangia

Abstract Currently, there is great emphasis, worldwide, on environmental issues. This will have an impact on civil aircraft design, manufacture and operation. Since the advent of the jet engine and swept wing aircraft, the trends have naturally tended towards greater productivity through increasing speed and payload. The cruise speed of conventional civil aircraft is unlikely to increase beyond current levels. Further increases in productivity are achieved by increasing payloads. This has led towards larger aircraft with the capability for increased ranges. It is shown that designing aircraft for longer ranges increases fuel burn significantly. A series of aircraft operational parameters have been analysed. Selected data and established trends for current and future aircraft are presented. The data has been interpreted into efficiency terms, relating payload, range, fuel consumed and a measure of unit costs. It is shown that ‘value’ (cost) and noise effective efficiencies decrease dramatically with increasing range. Environmental and economic considerations, in the future, may well demand greater efficiency in preference to productivity. One solution for long-range services is to use short-range hops. Another is via air-to-air refuelling. This will be addressed, in more detail, in a future paper.


Energy ◽  
2019 ◽  
Vol 176 ◽  
pp. 235-248
Author(s):  
David Alejandro Block Novelo ◽  
Uyioghosa Igie ◽  
Vinod Prakash ◽  
Artur Szymański

2011 ◽  
Vol 474-476 ◽  
pp. 1736-1739
Author(s):  
Yong Jie Zhang ◽  
Bin Tuan Wang

Blended-Wing-Body (BWB) civil aircraft possesses so light structure, high lift-drag ratio and low fuel burn that it has been an important topic of future civil aircraft. But internal pressure causes large bending stress instead of skin-membrane stress in BWB non-cylindrical fuselage. For 150 seats BWB fuselage, a composite 3-bay fuselage model is analyzed and two improved configurations of braced fuselage derivatives are designed in this paper. By optimization analysis, the optimized non-cylindrical fuselage structures are obtained in low bending stress and deformation condition, and optimized layer thicknesses ratio of composite material are presented. The optimization conclusions are very valuable and applicable for the fuselage structural design of BWB civil aircraft.


2007 ◽  
Vol 111 (1123) ◽  
pp. 589-592 ◽  
Author(s):  
R. K. Nangia

The aircraft industry, as a whole, is striving to limit its impact on the environment. Improved engine design and operation may offer a reduction in emissions of a few percent. More efficient air traffic control (ATC) may offer a limited reduction in overall fuel burn. Improvements in aerodynamic design and materials available (e.g. on A350XWB, B787) might achieve a few percent increases in efficiencies. The use of alternative fuels is some way off. The ACARE objectives present a stiff challenge. Our recent studies have shown that air-to-air-refuelling (AAR), well established in military circles, introduced to civil aircraft operations would provide fuel savings of the order of 30% – 40%. AAR will allow smaller (3,000nm range), more efficient (greener) aircraft, operating from shorter runways, to fulfil long-range route requirements. In addition, the ‘safety-net’ afforded by the availability of AAR will enable a host of hitherto borderline technologies to be accepted and utilised in future aircraft designs. Laminar flow will provide fuel savings and increased efficiency in its own right provided it is enabled within a civil AAR environment. Similarly, supersonic transport becomes an acceptable economic option.


Author(s):  
Hyun Sun Park ◽  
Norihiro Yamano ◽  
Kiyofumi Moriyama ◽  
Yu Maruyama ◽  
Yanhua Yang ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document