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Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles
Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition
Experimental Study of Aeroelastic Instability of Overexpanded Rocket Nozzle Extensions
Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets
Flow and Acoustic Fields of Rocket Jets Impinging on a Perforated Plate
Flow Structure Oscillations and Tone Production in Underexpanded Impinging Round Jets
Effects of Fluidic Oscillator Nozzle Angle on the Flowfield and Impingement Heat Transfer
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene
Hypersonic Boundary-Layer Instabilities due to Near-Critical Roughness
Effect of Port Corner Geometry on the Internal Performance of a Rotating-Vane-Type Thrust Reverser
Flow Control by Dielectric Barrier Discharge Actuators: Jet Mixing Enhancement
Optical Measurements of Transitional Events in a Mach-6 Boundary Layer
Numerical Study of the Dynamic Characteristics of Pintle Nozzles for Variable Thrust
Turbulence Model Effects on Cold-Gas Lateral Jet Interaction in a Supersonic Crossflow
Development of a Three-Dimensional Printed, Liquid-Cooled Nozzle for a Hybrid Rocket Motor
Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone