Combustor design trends for aircraft gas turbine engines
- Author(s):
- Sturgess, G.J. ( Innovative Scientific Solutions Inc., )
- Publication title:
- A.S.M.E. paper
- Title of ser.:
- ASME Technical Paper : TA
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-TA-29
- Paper no.:
- 96-TA-29
- Pub. info.:
- New York: The American Society of Mechanical Engineers
- Language:
- English
- Call no.:
- A11800
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Assessment of an abbreviated jet-A/JP-5/JP-8 reaction mechanism for modeling gas turbine engine gaseous emissions
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
CHARACTERIZATION OF REAL GAS PROPERTIES FOR SPACE SHUTTLE MAIN ENGINE FUEL TURBINE AND PERFORMANCE CALCULATIONS
National Aeronautics and Space Administration |
The American Society of Mechanical Engineers |
10
Technical Paper
Detailed Internal Measurements of a Siemens Combustor Operating at Gas Turbine Relevant Conditions.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Influences of airblast-atomizing fuel injector design on primary zone characteristics at blowout
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Design and Testing of a Unique, Compact Gas Turbine Catalytic Combustor Premixer.
American Society of Mechanical Engineers |