17 results
Abating CO2 and non-CO2 emissions with hydrogen propulsion
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- The Aeronautical Journal , First View
- Published online by Cambridge University Press:
- 02 April 2024, pp. 1-18
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Impact of tank gravimetric efficiency on propulsion system integration for a first-generation hydrogen civil airliner
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- The Aeronautical Journal / Volume 126 / Issue 1302 / August 2022
- Published online by Cambridge University Press:
- 10 June 2022, pp. 1324-1332
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Propulsion system integration for a first-generation hydrogen civil airliner?
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- The Aeronautical Journal / Volume 125 / Issue 1291 / September 2021
- Published online by Cambridge University Press:
- 28 May 2021, pp. 1654-1665
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Variable cycle jet engines for a Mach 2·7 supersonic civil transport
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- The Aeronautical Journal / Volume 102 / Issue 1011 / January 1998
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- 04 July 2016, pp. 31-36
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Predicted performance characteristics of a variable cycle turbofan
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- The Aeronautical Journal / Volume 101 / Issue 1006 / July 1997
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- 04 July 2016, pp. 263-268
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Performance simulation of a high-bypass turbofan with a 2D representation of the intake and fan components
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- The Aeronautical Journal / Volume 112 / Issue 1137 / November 2008
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- 03 February 2016, pp. 673-682
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The representation of GT component maps using Mach numbers
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- The Aeronautical Journal / Volume 111 / Issue 1121 / July 2007
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- 03 February 2016, pp. 453-460
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Experimental and computational investigation into the use of co-flow fluidic thrust vectoring on a small gas turbine
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- The Aeronautical Journal / Volume 112 / Issue 1127 / January 2008
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- 03 February 2016, pp. 17-25
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A method for calculating inlet distortion effects on stability of split-flow fans
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- The Aeronautical Journal / Volume 113 / Issue 1147 / September 2009
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- 03 February 2016, pp. 591-598
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Towards a full two dimensional gas turbine performance simulator
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- The Aeronautical Journal / Volume 111 / Issue 1121 / July 2007
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- 03 February 2016, pp. 433-442
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Analysis of turbine performance degradation effects due to geometry variations between actual components and design Intent
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- The Aeronautical Journal / Volume 114 / Issue 1159 / September 2010
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- 03 February 2016, pp. 569-578
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Evaluation of aero gas turbine preliminary weight estimation methods
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- The Aeronautical Journal / Volume 118 / Issue 1204 / June 2014
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- 27 January 2016, pp. 625-641
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Applying heat pipes to a novel concept aero engine: Part 1 – Design of a heat-pipe heat exchanger for an intercooled aero engine
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- The Aeronautical Journal / Volume 115 / Issue 1169 / July 2011
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- 27 January 2016, pp. 393-402
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Applying heat pipes to a novel concept aero engine: Part 2 – Design of a heat-pipe heat exchanger for an intercooled-recuperated aero engine
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- The Aeronautical Journal / Volume 115 / Issue 1169 / July 2011
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- 27 January 2016, pp. 403-410
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Flexible rotor blade dynamics for helicopter aeromechanics including comparisons with experimental data
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- The Aeronautical Journal / Volume 119 / Issue 1213 / March 2015
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- 27 January 2016, pp. 301-342
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Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics
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- The Aeronautical Journal / Volume 118 / Issue 1206 / August 2014
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- 27 January 2016, pp. 861-901
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Total pressure distortion levels at the aerodynamic interface plane of a military aircraft
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- The Aeronautical Journal / Volume 119 / Issue 1219 / September 2015
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- 27 January 2016, pp. 1147-1166
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