Environmental Engineering Reference
In-Depth Information
Mongia HC (2010b) Correlations for gaseous emissions of aero-propulsion engines from sea-level
to cruise operation. AIAA paper 2010-1530
Mongia HC (2011a) Engineering aspects of complex gas turbine combustion mixers part I: high
Δ T. AIAA paper 2011-107
Mongia HC (2011b) Engineering aspects of complex gas turbine combustion mixers part II: high
T 3 . AIAA paper 2011-106
Mongia HC (2011c) Engineering aspects of complex gas turbine combustion mixers part III:
30 OPR. AIAA paper 2011-5525
Mongia HC (2011d) Engineering aspects of complex gas turbine combustion mixers part IV: swirl
cup. AIAA paper 2011-5526
Mongia HC (2011e) Engineering aspects of complex gas turbine combustion mixers part V:
40 OPR. AIAA paper 2011-5527
Mongia HC (2013a) N+ 3 and N+ 4 generation aeropropulsion engine combustors part 1: large
engines
emissions. GT2013-94570
Mongia HC (2013b) N+ 3 and N+ 4 generation aeropropulsion engine combustors part 2: medium
size rich-dome engines and lean-domes. GT2013-94571
Mongia HC (2013c) N+ 3 and N+ 4 Generation aeropropulsion engine combustors part 3: small
engine emissions and axial staging combustion technology. GT2013-94572
Mongia HC (2013d) N+ 3 and N+ 4 generation aeropropulsion engine combustors part 5: NO x ,
CO, HC and smoke emissions. AIAA paper 2013-3653
Mongia HC (2013e) N+ 3 and N+ 4 generation aeropropulsion engine combustors part 6:
operating conditions, target goals and lifted jets. AIAA paper 2013-3654
Mongia HC, Ambs LL (1974) A model for the combustion and extinction of composite solid
propellants during depressurization. Combust Flame 22:59
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69
Mongia HC, Smith KF (1978) An empirical/analytical design methodology for gas turbine
combustor. AIAA Paper 78-998
Mongia HC, Reynolds RS, Srinivasan R (1986) Multidimensional gas turbine combustion
modeling: applications and limitations. AIAA J 24(6):890
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904
Mongia HC, Held TJ, Hsiao GC, Pandalai RP (2003) Challenges and progress in controlling
dynamics in gas turbine combustors. J Propul Power 19:822
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829
Mongia H, Hsiao G, Burrus D, Sreedhar PSVS, Rao A, Naik P (2004a) Combustor diffuser
modeling part I: inlet pro les and 2-D calculations. AIAA paper 2004-4168
Mongia H, Hsiao G, Burrus D, Sreedhar PSVS, Rao A (2004b) Combustor diffuser modeling part
II: inlet pro les and 3-D calculations. AIAA paper 2004-4169
Mongia H, Hsiao G, Burrus D, Habeeb K, Sreedhar PSVS (2004c) Combustor diffuser modeling
part III: validation w/typical separating single passage diffusers combustor diffuser modeling.
AIAA paper 2004-4170
Mongia H, Hsiao G, Burrus D, Sreedhar PSVS, Rao A (2004d) Combustor diffuser modeling part
IV: effect of cowling geometry, mixer size and nozzle blockage. AIAA paper 2004-4171
Mongia H, Hsiao G, Ravindra MVV, Sreedhar PSVS (2004e) Combustor diffuser modeling part
V: validation with a three passage diffuser rig data. AIAA paper 2004-4172
Mongia H, Hsiao G, Mueller M, Dai Z, Ravindra MVV, Sreedhar PSVS, Arvind P (2004f)
Combustor diffuser modeling part VI: validation with a four passage diffuser rig data. AIAA
paper 2004-4173
Mongia HC, Held TJ, Hsiao GC, Pandalai RP (2005) Incorporation of combustion instability
issues into design process: GE aeroderivative and aero engines experience. In: Lieuwen TC,
Yang V (eds) Progress in astronautics and aeronautics, vo 210. pp 43
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64
Moses CA, Roets PN (2008) Properties, characteristics and combustion performance of SASOL
fully synthetic jet fuel. GT2008-50545
Murthy SNB, Mongia HC (1969) Progressive acoustic and weak shock waves in AI, Be and B
flames. AIAA paper 1969-540
Nealy DA, Reider SB, Mongia HC (1985) Alternate cooling con guration for gas turbine
combustion systems. In: AGARD CP-390, pp 25-1 - 25-15
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