Character and interface shear strength of accreted ice on subcooled surfaces submerged in fuel.
- Published in:
- Aeronautical Journal, 2015, v. 119, n. 1221, p. 1377, doi. 10.1017/S0001924000011301
- By:
- Publication type:
- Article
Works matching DE "AIRPLANE fuel systems"
Results: 12
1
2
Lead Memory in General Aviation Aircraft Engine Emissions.
- Published in:
- Journal of Aviation Technology & Engineering, 2012, v. 1, n. 2, p. 74, doi. 10.5703/1288284314660
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- Publication type:
- Article
3
Efficiency Paradox.
- Published in:
- Tribology & Lubrication Technology, 2014, v. 70, n. 8, p. 6
- By:
- Publication type:
- Article
4
THE POWER OF AIRCRAFT HYDRAULIC REDUNDANCY SYSTEMS.
- Published in:
- Tribology & Lubrication Technology, 2013, v. 69, n. 6, p. 40
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- Publication type:
- Article
5
Learning from aircraft fuel tank explosions.
- Published in:
- Loss Prevention Bulletin, 2008, n. 203, p. 3
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- Publication type:
- Article
6
NATIONAL AIRLINES FUEL MANAGEMENT AND ALLOCATION MODEL.
- Published in:
- Interfaces, 1977, v. 7, n. 2, p. 1, doi. 10.1287/inte.7.2.1
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- Publication type:
- Article
7
Effects of TRiEGME on water icing behavior in aviation turbine fuel.
- Published in:
- Asia-Pacific Journal of Chemical Engineering, 2016, v. 11, n. 1, p. 118, doi. 10.1002/apj.1949
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- Publication type:
- Article
8
Failure prognosis of multiple uncertainty system based on Kalman filter and its application to aircraft fuel system.
- Published in:
- Advances in Mechanical Engineering (Sage Publications Inc.), 2016, v. 8, n. 10, p. 1, doi. 10.1177/1687814016671445
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- Publication type:
- Article
9
Transient Process of Helicopter Fuel System Transferred from Boost Fueling to Self-Suck.
- Published in:
- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 6, p. 895
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- Publication type:
- Article
10
DESIGN AND OPTIMISATION OF FUEL TANKS FOR BWB CONFIGURATIONS.
- Published in:
- Archive of Mechanical Engineering, 2016, v. 63, n. 4, p. 605, doi. 10.1515/meceng-2016-0034
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- Publication type:
- Article
11
GROUND TEST FACILITY FOR A TURBOSHAFT-TYPE APU TG-16M FOR PASSENGER AIRCRAFT.
- Published in:
- Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 85, doi. 10.19062/2247-3173.2016.18.1.11
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- Publication type:
- Article
12
STUDY OF THE TURBOJET ENGINES AS PROPULSION SYSTEMS FOR THE UNMANNED AERIAL VEHICLES.
- Published in:
- Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 115, doi. 10.19062/2247-3173.2016.18.1.15
- By:
- Publication type:
- Article