Investigations of Shock Boundary Layer Interactions Over a Soft Material for Separated Control

von Walz, James R.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Fluid dynamics ; Volume 4 of 7 (2022)

Effects of Pressure Sensitive Paint on the Dynamics of Half-Inlet Shock Dynamics

von Jenquin, Chase
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) High-speed air-breathing propulsion (2022)

Half-Isolator Shock Dynamics Due to the Presence of Pressure-Sensitive Paint and Microramp Vortex Generators

von Jenquin, Chase
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Aerodynamic measurement technology ; Volume 2 of 2 (2023)

Experimental Investigations of the Hypersonic Streamtraced Performance Inlet at Sub-Design Mach Number and Varying Angles of Attack

von Schram, Matthew J.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Inlets, nozzles, and propulsion systems integration (2023)

IMPACT OF PANEL VIBRATIONS ON THE DYNAMIC FIELD PROPERTIES IN SUPERSONIC FLOW

von Varigonda, Santosh Vaibhav
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Fluid dynamics ; Volume 2 of 2 (2021)

Experimental Investigations of the Hypersonic Streamtraced Performance Inlet at Sub-Design Mach Number and Varying Angles of Attack

von Schram, Matthew J.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) High-speed air-breathing propulsion (2023)

SIMULTANEOUS MEASUREMENT OF PRESSURE AND VELOCITY FIELDS OF AN OBLIQUE SBLI ON A FLEXIBLE PANEL USING PIV AND PSP

von Varigonda, Santosh Vaibhav
Veröffentlicht in AIAA Aviation Forum (2020 : Online) Fluid dynamics ; Volume 2 of 3 (2020)

MIXTURE FRACTION IMAGING OF DISTRIBUTED REGIME TURBULENT JET FLAME USING RAYLEIGH SCATTERING

von Sahoo, Abinash
Veröffentlicht in AIAA Aviation Forum (2020 : Online) Plasmadynamics and lasers (2020)

2D VELOCITY FIELD MEASUREMENT OF CONVENTIONAL AND DISTRIBUTED REGIME TURBULENT JET FLAME USING PARTICLE IMAGE VELOCIMETRY

von Sahoo, Abinash
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) Propellants and combustion (2021)

NUMERICAL INVESTIGATION OF PASSIVE FLOW CONTROL USING PERMEABLE AND WAVY WALLS IN OBLIQUE SHOCK WAVE BOUNDARY LAYER INTERACTION

von Bharadwaj, Anand S.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Applied aerodynamics ; Volume 4 of 5 (2021)

INVESTIGATIONS OF MIXED CONVENTIONAL AND MILD COMBUSTION FLAMES

von Narayanaswamy, Venkateswaran
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) High-speed air-breathing propulsion (2020)

Development and Testing of High-Temperature Fast Response Pressure Sensitive Paint

von Wood, Sam J.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Aerodynamic measurement technology ; Volume 1 of 2 (2023)

Mach 4 Performance of a Hypersonic Streamtraced Inlet - Part 1: Experimental Investigations

von Johnson, Ethan
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) High-speed air-breathing propulsion (2022)

Mach 4 Performance of a Hypersonic Streamtraced Inlet - Part 2: Computational Results

von Mccready, Jonathan
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) High-speed air-breathing propulsion (2022)

EFFECTS OF THREE-DIMENSIONAL PRESSURE GRADIENTS ON HIGH-SPEED TURBULENT BOUNDARY LAYERS

von Peltier, Scott J.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Structural dynamics ; Volume 1 of 2 (2021)

FLOW DISTORTION COMPUTATIONAL MODELING AND DESIGN OPTIMIZATION FOR SUPERSONIC INLET

von Boles, John A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Inlets, nozzles, and propulsion systems integration (2021)

FLOW DISTORTION COMPUTATIONAL MODELING AND DESIGN OPTIMIZATION FOR SUPERSONIC INLET

von Boles, John A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Applied aerodynamics ; Volume 3 of 5 (2021)

EFFECTS OF THREE-DIMENSIONAL PRESSURE GRADIENTS ON HIGH-SPEED TURBULENT BOUNDARY LAYERS

von Peltier, Scott J.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Applied aerodynamics ; Volume 3 of 5 (2021)

ANALYSIS OF TURBULENCE MODELS TO PREDICT FIN-ON-CYLINDER SHOCK BOUNDARY LAYER INTERACTIONS

von Pickles, Joshua
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 5 of 7 (2020)

Investigations of the Transition Between Conventional and Distributed Regime in Turbulent Jet Flames

von DeBoskey, Ryan D.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Propellants and combustion ; Volume 2 of 2 (2022)