SPOD Analysis of Pulsed Jets in Supersonic Crossflow Using a High Frequency Actuator: An Abstract

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

NUMERICAL INVESTIGATION OF PULSED JETS IN SUPERSONIC CROSSFLOW USING A HIGH FREQUENCY ACTUATOR

von Castelino, Neil
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) High-speed air-breathing propulsion (2021)

NATURE OF FLOW FIELD & ACOUSTICS OF TWIN SUPERSONIC RECTANGULAR JETS

von Karnam, Aatresh
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Aeroacoustics (2020)

COMPARISON OF FLOW CHARACTERISTICS OF SINGLE AND TWIN RECTANGULAR JETS USING OVERFLOW CODE

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

EFFECTS OF SWIRL NUMBER AND CENTRAL ROD ON FLOW IN LEAN PREMIXED SWIRL COMBUSTER

von Yellugari, Kranthi
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Propellants and combustion ; Volume 1 of 2 (2020)

NUMERICAL INVESTIGATION OF A SWIRL INDUCED FLAMELESS COMBUSTOR FOR GAS TURBINE APPLICATIONS

von Sharma, Anshu
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Gas turbine engines (2021)

INVESTIGATION OF LONGITUDINAL OPERATING MODES IN ROTATING DETONATION COMBUSTORS

von Bluemner, Richard
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion (2020)

STUDY OF TEMPERATURE EFFECT ON FLOW AND ACOUSTIC BEHAVIOR OF SUPERSONIC JET EMANATING FROM A FACETED NOZZLE

von Rodriguez, Omar Lopez
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Aeroacoustics (2021)

Implementation of Chevrons as a Noise Reduction System for a Supersonic Tactical Nozzle

von Rodriguez, Omar Lopez
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Aeroacoustics (2022)

ANALYSIS OF RDC OPERATION BY DYNAMIC MODE DECOMPOSITION (DMD)

von Bohon, Myles
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Pressure gain combustion (2019)

Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors

von Barnouin, Provence
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)

CHARACTERIZATION AND EXAMINATION OF PERFORMANCE PARAMETERS OF BACK-PRESSURIZED RDCS

von Geller, Alexander C.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion (2020)

Effect of Axial Location of Micro Vortex Generators on Supersonic Jet Noise Reduction

von Liu, Junhui
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Aeroacoustics (2022)

EFFECT OF NOZZLE SPACING ON FLOW BEHAVIOR IN A LEAN DIRECT INJECTION COMBUSTOR

von Yellugari, Kranthi
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Propellants and combustion ; Volume 1 of 2 (2021)

NOISE CHARACTERISTICS OF LOW ASPECT RATIO SUPERSONIC TWIN JET CONFIGURATION

von Viswanath, Kamal
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Aeroacoustics (2020)

Enhanced Supersonic Jet Noise Reduction Using Two Array Configurations of Micro Vortex Generators

von Saleem, Mohammad
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Aeroacoustics (2022)

The Effects of Aerogel Lining on a H2-Air Fueled Annular RDC Combustor

von Betancourt, Jorge J.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)

Simultaneous Shadowgraph and Chemiluminescence Measurements of a Reactive Flow-Through Rotating Detonation Combustor

von Wiggins, Rachel
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)

Thermoacoustic Suppression in a Rotating Detonation Combustion Using Perforated Liner

von Pritschau, Tyler C.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)

CHARACTERIZATION OF NON-REACTING SWIRLING FLOW IN A GAS TURBINE FUEL INJECTOR

von Ghulam, Mohamad M.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Gas turbine engines (2021)