Some unconventional aero gas turbines using hydrogen fuel

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 2 B, Issue , 2002, Pages 683-690

  Boggia, Stefano ^a   Jackson, Anthony ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERO GAS TURBINES; CRYOGENIC PROPERTIES;

AIRCRAFT FUELS; FUEL CONSUMPTION; HYDROGEN FUELS; LOW TEMPERATURE PROPERTIES; NOZZLES; TAKEOFF; TURBOFAN ENGINES;

GAS TURBINES;

EID: 0036998257     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30412     Document Type: Conference Paper

References (10)

1. "Analysis of several methane-fueled engine cycles for Mach 3.0 flight", NASA TN D-4699, 1968
2. "Analysis of a Topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel", NASA TP-2294, 1997
3. McCarty, R.D., "Hydrogen: its technology and implications" Volume 3: "Hydrogen properties", CRC Press, 1975
4. "Coefficients for calculating Thermodynamic and Transport Properties of Individual Species", NASA TM 4513, 1993
5. Boggia, S., "Novel concepts for aero gas turbine engines burning hydrogen - Cryoplane", Thesis, Cranfield University, 2000
6. Brewer, G.D., "Hydrogen Aircraft technology", CRC Press, 1991
7. Kurzke, J., GasTurb, http://www.gasturb.de
8. Boggia, Jackson, Singh: "Unconventional cycles for aero gas turbine engines burning hydrogen", ISOABE Conference proceedings, September 2001
9. Boggia, S., "Four Unconventional Aero Gas Turbine Engines Burning Hydrogen - Cryoplane Project", Thesis, Cranfield University, 2001
10. Cryoplane Website, http://www.cryoplane.com