publication venue for
- Modern Competing Flames Model for Composite Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Propellant Combustion. 39:675-687. 2023
- Very-High-Pressure Burning Rates of Aluminized and Nonaluminized AP/HTPB-Composite Propellants. 37:693-700. 2021
- Plasma-Assisted Fuel Atomization and Multipoint Ignition for Scramjet Engines. 36:357-362. 2020
- Aging Effects on the Burning Rates of Composite Solid Propellants with Nano-Additives. 35:342-351. 2019
- Mathematical Model of Dual-Pulse Laser Ignition. 34:408-414. 2018
- Control of shock-wave/boundary-layer interaction using nanosecond-pulsed plasma actuators. 34:909-919. 2018
- Aerothermal Optimization and Experimental Verification for Discrete Turbine Airfoil Film Cooling. 31:543-558. 2015
- Miniaturized Combustor for Supersonic Methane-Air Flames. 30:1167-1174. 2014
- Oxidation of Ethylene-Air Mixtures at Elevated Pressures, Part 1: Experimental Results. 30:790-798. 2014
- Assessing the mixedness of composite solid rocket propellants using fluorescent particles. 26:987-992. 2010
- Performance of Ammonium-Perchlorate-Based Composite Propellant Containing Nanoscale Aluminum. 26:461-466. 2010
- Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow. 26:373-376. 2010
- Supersonic Boundary-Layer Combustion: Effects of Upstream Entropy and Shear-Layer Thickness. 26:57-66. 2010
- Detached-Eddy Simulation of a Louver-Cooling Scheme for Turbine Blades. 24:1133-1140. 2008
- Single-cycle impulse from detonation tubes with nozzles. 24:81-87. 2008
- Ignition and oxidation of lean CO/H2 fuel blends in air. 23:1291-1303. 2007
- Flowfield studies of a diamond-shaped fuel injector in a supersonic flow. 23:1168-1176. 2007
- Simulation of transverse gaseous injection through diamond ports into supersonic freestream. 23:772-782. 2007
- Film-cooling effectiveness on squealer cavity and rim walls of gas-turbine blade tip. 22:889-899. 2006
- Turbine blade internal cooling passages with rib turbulators. 22:226-248. 2006
- Detonation tube impulse in subatmospheric environments. 22:845-851. 2006
- Unsteady quasi-one-dimensional nonlinear dynamc model of supersonic through-flow fan surge. 22:188-196. 2006
- Ignition and oxidation of ethylene-oxygen-diluent mixtures with and without silane. 21:1045-1056. 2005
- Reply to Comment on "Analytical Model for the Impulse of Single Cycle Pulse Detonation Tube" by M. I. Radulescu and R. K. Hanson. 20:957-959. 2004
- Reflected-shock ignition of SiH4/H2/O2/Ar and SiH4/CH4/O2/Ar mixtures. 20:665-674. 2004
- Effect of porous thrust surfaces on detonation transition and detonation tube impulse. 20:811-819. 2004
- Erratum for "Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube". 20:765-767. 2004
- Impulse correlation for partially filled detonation ibbes. 20:947-950. 2004
- Reply to Comment on "Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube" by W.H. Heiser and D.T. Pratt. 20:189-191. 2004
- Sonic injection into a Mach 5.0 freestream through diamond orifices. 20:280-287. 2004
- Active control of compressor instability and surge by stator blades adjustment. 19:312-317. 2003
- Analytical model for the impulse of single-cycle pulse detonation tube. 19:22-38. 2003
- Massively Parallel Simulation of the Unsteady Flow in an Axial Turbine Stage. 18:465-471. 2002
- Direct experimental impulse measurements for detonations and deflagrations. 18:1033-1041. 2002
- Development and Validation of a Massively Parallel Flow Solver for Turbomachinery Flows. 17:659-668. 2001
- Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream. 16:234-242. 2000
- Comment on "Shock-loss model for transonic and supersonic axial compressors with curved blades" - Reply by the author to N. A. Cumpsty and C. Freeman. 16:168-168. 2000
- Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers. 16:153-154. 2000
- Reply by the Author to N. A. Cumpsty and C. Freeman. 16:168-168. 2000
- Reduced kinetics mechanisms for ram accelerator combustion. 15:591-600. 1999
- Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume. 15:432-439. 1999
- Ignition delay times of ram accelerator CH4/O2/diluent mixtures. 15:82-91. 1999
- Shock-loss model for transonic and supersonic axial compressors with curved blades. 14:470-478. 1998
- Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers. 14:110-118. 1998
- Hybrid friction-impact vibration damper for cryogenic rotating machinery. 13:495-501. 1997
- Stability of projectiles in thermally choked ram accelerators. 12:807-809. 1996
- Performance characterization of a highly offset diffuser with vortex generator jets. 12:237-244. 1996
- THERMOHYDRODYNAMIC ANALYSIS OF FLUID FILM BEARINGS FOR CRYOGENIC APPLICATIONS. 11:964-972. 1995
- NONLINEAR DYNAMIC SIMULATION OF SINGLE-SPOOL AND MULTISPOOL CORE ENGINES .2. SIMULATION, CODE VALIDATION. 10:863-867. 1994
- ROTORDYNAMIC COEFFICIENT TEST-RESULTS FOR A 4-STAGE BRUSH SEAL. 9:462-465. 1993
- Cascade flow calculations by a multigrid Euler method. 9:90-97. 1993
- Acoustic-vortex interactions and low-frequency oscillations in axisymmetric combustors. 5:165-171. 1989
- Numerical simulations of acoustic-vortex interactions in a central-dump ramjet combustor. 3:525-533. 1987
- Experimental Validation of a Pulse-Modulated Flow-Control Actuator for Turbomachinery. 33:1358-1368.
- Proper Orthogonal Decomposition of Turbine Rotor-Stator Interaction. 19:268-281.
- Three-Dimensional Hybrid Mesh Generation for Turbomachinery Airfoils. 18:536-543.
- Burning Rate Characterization of Ammonium Perchlorate Pellets Containing Micro- and Nano-Catalytic Additives 2022
- Control of Shock-Wave/Boundary-Layer Interaction Using Nanosecond-Pulsed Plasma Actuators 2018
- Temperature Sensitivity of Composite Propellants Containing Novel Nano-Additive Catalysts 2018
- Assessing the Mixedness of Composite Solid Rocket Propellants Using Fluorescent Particles 2010
- Nano Additives and Plateau Burning Rates of Ammonium-Perchlorate-Based Composite Solid Propellants 2009
- Dynamic simulation of a wave-rotor-topped turboshaft engine 2000
- Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers 1998
- NONLINEAR DYNAMIC SIMULATION OF SINGLE-SPOOL AND MULTISPOOL CORE ENGINES .1. COMPUTATIONAL METHOD 1994
- Three-Dimensional Hybrid Mesh Generation for Turbomachinery Airfoils