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Foreword | ||
Sect. 1 | Control of combustion processes | 1 |
Ch. 1 | Simultaneous velocity and temperature field measurements of a jet flame | 3 |
Ch. 2 | Infrared absorption tomography for active combustion control | 9 |
Ch. 3 | Deterministic and probabilistic approaches for prediction of two-phase turbulent flow in liquid-fuel combustors | 21 |
Ch. 4 | Large-scale simulations of turbulent combustion and propulsion systems | 31 |
Ch. 5 | Direct simulation of primary atomization | 39 |
Ch. 6 | Extinction and relight in opposed premixed flames | 49 |
Ch. 7 | Influence of Markstein number on the parametric acoustic instability | 65 |
Ch. 8 | Prevaporized JP-10 combustion and the enhanced production of turbulence using countercurrent shear | 75 |
Ch. 9 | Mixing control for jet flows | 87 |
Ch. 10 | Characteristics and control of a multiswirl spray combustor | 97 |
Ch. 11 | Swirling jet systems for combustion control | 111 |
Ch. 12 | Control of flame structure in spray combustion | 129 |
Ch. 13 | Porous media burners for clean engines | 139 |
Ch. 14 | Simulations of a porous burner for a gas turbine | 145 |
Ch. 15 | Characteristics and control of combustion instabilities in a swirl-stabilized spray combustor | 157 |
Ch. 16 | Combustion and mixing control studies for advanced propulsion | 169 |
Ch. 17 | Active pattern factor control on an advanced combustor | 181 |
Ch. 18 | System design methods for simultaneous optimal control of combustion instabilities and efficiency | 191 |
Ch. 19 | Model-based optimal active control of liquid-fueled combustion systems | 201 |
Sect. 2 | High-speed jet noise | 211 |
Ch. 1 | Aeroacoustics and emissions studies of swirling combustor flows | 213 |
Ch. 2 | Considerations for the measurement of very-high-amplitude noise fields | 223 |
Ch. 3 | High-speed jet noise reduction using microjets | 231 |
Ch. 4 | Acoustic test flight results with prediction for military aircraft during FCLP mission | 245 |
Ch. 5 | Computational fluid dynamics simulations of supersonic jet-noise reduction concepts | 259 |
Sect. 3 | Pulse detonation engines | 271 |
Ch. 1 | Investigation of spray detonation characteristics using a controlled, homogeneously seeded, two-phase mixture | 273 |
Ch. 2 | Deflagration-to-detonation studies for multicycle PDE applications | 283 |
Ch. 3 | Initiator diffraction limits in a pulse detonation engine | 293 |
Ch. 4 | The role of geometrical factors in deflagration-to-detonation transition | 305 |
Ch. 5 | Pseudospark-based pulse generator for corona-assisted combustion experiments | 315 |
Ch. 6 | Breakup of droplets under shock impact | 321 |
Ch. 7 | Impulse production by injecting fuel-rich combustion products in air | 329 |
Ch. 8 | Thermodynamic evaluation of the dual-fuel PDE concept | 341 |
Ch. 9 | Thermal decomposition of JP-10 studied by microflow tube pyrolysis-mass spectrometry | 355 |
Ch. 10 | Laser diagnostics and combustion chemistry for pulse detonation engines | 365 |
Ch. 11 | Computational studies of pulse detonation engines | 377 |
Ch. 12 | Simulation of direct initiation of detonation using realistic finite-rate models | 389 |
Ch. 13 | System performance and thrust chamber optimization of air-breathing pulse detonation engines | 397 |
Ch. 14 | Software development for automated parametric study and performance optimization of pulse detonation engines | 407 |
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