Design of aircraft

von Corke, Thomas C.
Veröffentlicht 2003

SEPARATION CONTROL IN 2-D CLOSED CHANNEL BEND

von Samper, Thomas C.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 3 of 7 (2020)

A.C. PLASMA ANEMOMETER MEASUREMENTS IN A SUPERSONIC HYDROGEN JET

von Matlis, Eric H.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Pressure gain combustion (2021)

A.C. PLASMA ANEMOMETER MEASUREMENTS IN A SUPERSONIC HYDROGEN JET

von Matlis, Eric H.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Plasmadynamics and lasers (2021)

Wind energy design

von Corke, Thomas C.
Veröffentlicht 2018

A.C. PLASMA ANEMOMETER MEASUREMENTS IN A SUPERSONIC HYDROGEN JET

von Matlis, Eric H.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Aerodynamic measurement technology ; Volume 2 of 2 (2021)

Boundary Layer Turbulence Characteristics and Mechanisms Due to Drag Reduction Initial Conditions

von Myers, Andrew
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 1 of 3 (2022)

CHARACTERISTICS OF DRAG REDUCED TURBULENT BOUNDARY LAYERS THROUGH PULSED-DC ACTUATION

von Duong, Alan H.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 1 of 7 (2020)

CONTROLLED STATIONARY/TRAVELING CROSS-FLOW MODE INTERACTION IN MACH 6 BOUNDARY LAYER

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

Single Electrode A.C. Plasma Anemometer in High Speed H2 Jet with Background RF Plasma

von Matlis, Eric H.
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Plasmadynamics and lasers (2022)

Experimental Characterization of Smooth Body Flow Separation Over Wall-Mounted Gaussian Bump

von Gray, Patrick D.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Fluid dynamics ; Volume 5 of 7 (2022)

Benchmark Characterization of Separated Flow Over Smooth Gaussian Bump

von Gray, Patrick D.
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 1 of 3 (2022)

DESIGN OF A HYPERSONIC BOUNDARY LAYER TRANSITION CONTROL EXPERIMENT UTILIZING A SWEPT FIN CONE GEOMETRY IN MACH 6 FLOW

von Middlebrooks, John B.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Fluid dynamics ; Volume 3 of 6 (2021)

Cross-Flow Instability Experiments on a Swept Fin-Cone with Variable Nose Bluntness in Mach 6 Flow

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