-
1
-
-
0003677534
-
-
IPCC: Penner, J.E., Lister, D.H., Griggs, D.J., Dokken, D.J., and McFarland, M. (eds.); Cambridge University Press, Cambridge, U.K
-
IPCC: Penner, J.E., Lister, D.H., Griggs, D.J., Dokken, D.J., and McFarland, M. (eds.), Aviation and the Global Atmosphere A Special Report of IPCC working Groups I and III, 1999, Cambridge University Press, Cambridge, U.K
-
(1999)
Aviation and the Global Atmosphere A Special Report of IPCC Working Groups I and III
-
-
-
2
-
-
0013418825
-
Aviation and the changing climate
-
Miake-Lye R., Waitz, I., Fahey D., Wesoky, H., and Wey, C., 2000, "Aviation and the Changing Climate," Aerospace America, Vol. 38, pp. 35-39.
-
(2000)
Aerospace America
, vol.38
, pp. 35-39
-
-
Miake-Lye, R.1
Waitz, I.2
Fahey, D.3
Wesoky, H.4
Wey, C.5
-
3
-
-
0013420712
-
Ultra lean combustion at high inlet temperatures
-
ASME Paper 81-GT-44
-
Anderson, D.N., 1981, "Ultra Lean Combustion at High Inlet Temperatures," ASME Paper 81-GT-44, Gas Turbine Conference & Products Show, Houston TX, 1981
-
(1981)
Gas Turbine Conference & Products Show, Houston TX, 1981
-
-
Anderson, D.N.1
-
4
-
-
3342897970
-
Lean low NOx primary zones using radial swirlers
-
paper ASME 88-GT-245
-
Alkabie, H.S., Andrews, G.E., and Ahmad, N.T, 1988, "Lean Low NOx Primary Zones Using Radial Swirlers," paper ASME 88-GT-245, ASME Gas Turbine and Aero Engine Congress and Exposition, Amsterdam, 1988.
-
(1988)
ASME Gas Turbine and Aero Engine Congress and Exposition, Amsterdam, 1988
-
-
Alkabie, H.S.1
Andrews, G.E.2
Ahmad, N.T.3
-
5
-
-
0032285768
-
A liquid fueled, lean burn, gas turbine combustor injector
-
Schaefer, S. W., and Samuelsen,G. S., 1998, "A Liquid Fueled, Lean Burn, Gas Turbine Combustor Injector," Combustion Science and Technology, Vol. 139, pp. 41-47
-
(1998)
Combustion Science and Technology
, vol.139
, pp. 41-47
-
-
Schaefer, S.W.1
Samuelsen, G.S.2
-
7
-
-
0011931818
-
Low NOx potential of gas turbine engines
-
AIAA Paper 90-0550
-
Tacina, R. R., 1990, "Low NOx Potential of Gas Turbine Engines," AIAA Paper 90-0550, 28th Aerospace Science Meeting, Reno NV, 1990
-
(1990)
28th Aerospace Science Meeting, Reno NV, 1990
-
-
Tacina, R.R.1
-
8
-
-
84885289897
-
Integrated fuel injection and mixing system with impingement cooling face
-
Patent pending
-
Mansour, A, Laing, P., Harvey, R. and Tacina, R, 2001, "Integrated Fuel Injection and Mixing System with Impingement Cooling Face," Patent pending.
-
(2001)
-
-
Mansour, A.1
Laing, P.2
Harvey, R.3
Tacina, R.4
-
9
-
-
0013328104
-
A low NOx lean-direct injection, multipoint integrated module combustor concept for advanced aircraft gas turbines
-
Tacina, R., Wey, C., Laing, P., Mansour, A, 2001, "A Low NOx Lean-Direct Injection, MultiPoint Integrated Module Combustor Concept for Advanced Aircraft Gas Turbines," Clean Air Conference, Porto, Portugal
-
(2001)
Clean Air Conference, Porto, Portugal
-
-
Tacina, R.1
Wey, C.2
Laing, P.3
Mansour, A.4
-
11
-
-
0004251733
-
-
Taylor and Francis, Philadelphia, PA
-
Lefebvre, A. H., 1998. Gas Turbine Combustion, Second Edition, Taylor and Francis, Philadelphia, PA, p.217
-
(1998)
Gas Turbine Combustion, Second Edition
, pp. 217
-
-
Lefebvre, A.H.1
-
12
-
-
0013374379
-
Procedure for the calculation of gaseous emissions from aircraft turbine engines
-
SAE ARP1533
-
SAE ARP1533 - 1996, "Procedure for the Calculation of Gaseous Emissions from Aircraft Turbine Engines".
-
(1996)
-
-
-
13
-
-
0013328487
-
A high pressure and high temperature NOx correlation
-
paper in progress
-
Wey,C., 2002, "A High Pressure and High Temperature NOx Correlation," paper in progress
-
(2002)
-
-
Wey, C.1
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