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Effects of cavitation in common-rail diesel nozzles on the mixing process
Numerical analysis of flow separation and side loads of a conical nozzle during staging
Pose measurement of nozzle based on laser range finders for capturing satellite
Experimental investigation of single expansion ramp performance
Experimental and computational investigation of double serpentine nozzle
Corrugated right-angled triangular tabs for supersonic jet control
New features of solid particle erosion damage of control stage blades in supercritical steam turbine
Numerical analysis of gas turbine inlet fogging nozzle manifold resistance
Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle
Measurements of Hub Flow Interaction on Film Cooled Nozzle Guide Vane in Transonic Annular Cascade
Flow and Acoustics of Clustered Rockets During Startup
Effect of Nozzle Spacing on Nitrogen-Oxide Emissions and Lean Operability
Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle
Spatial Stability Analysis of Subsonic Jets Modified for Low-Frequency Noise Reduction
Visualization analysis of relationship between vortex flow and cavitation behavior in diesel nozzle
Subsonic Jet Noise Simulations Using Both Structured and Unstructured Grids
Modeling Free Shock Separation Induced Side Loads in Overexpanded Rocket Nozzles
Inverse diffusion and partially premixed flames with elliptical/swirling- and cross-flows
Analysis of Plume Infrared Signatures of S-Shaped Nozzle Configurations of Aerial Vehicle
Obituaries: AIAA Fellow Leavitt Died in June
Thermodynamic losses of hetero and homogeneous condensation in steam turbine cascades
How the Nozzle Geometry Impacts Vortex Breakdown in Compressible Swirling-Jet Flows
Navier–Stokes Simulation of Graphite Nozzle Erosion at Different Pressure Conditions
Development of a Short-Duration Rocket Nozzle Flow Simulation Facility
Hot-Flow Simulation of Aeroacoustics and Suppression by Water Injection During Rocket Liftoff
Reaction Control Thruster Thermal Design for a Mission to Mercury
Design study of Coanda devices for transonic circulation control