Analysis of essential patent portfolios via bibliometric mapping : an illustration of leading firms in the 4G era

von Han, Yoo-Jin
Veröffentlicht in Technology analysis & strategic management (2015)

The effects of the characteristics of Korean firms on the patent production function

von Han, Yoo-jin
Veröffentlicht in Economics of innovation and new technology (2007)

Low Order Analysis of Panel Vibration Under Ramp-Induced Shock / Boundary Layer Interaction

von Eitner, Marc A.
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 2 of 3 (2022)

Unsteadiness in Shock/Boundary-Layer Interaction Over a Compliant Panel at Mach 2

von Musta, Mustafa N.
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 3of 3 (2022)

Effect of Structural Modifications on Vibratory Response of Panel Under Ramp-Induced Shock Wave Boundary Layer Interaction

von Eitner, Marc A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Dynamics specialists ; Volume 1 of 2 (2022)

INVESTIGA TION OF FLOW-STRUCTURE COUPLING FOR A COMPLIANT PANEL UNDER A SHOCK/BOUNDARY-LA YER INTERACTION USING FAST-RESPONSE PSP

von Musta, Mustafa N.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Fluid dynamics ; Volume 2 of 2 (2021)

Unsteadiness of Mach 5 Ramp-Induced Shock-Wave/Boundary-Layer Interaction Using 100 kHz Time-Resolved PIV and 20 kHz Fast-Response PSP

von Ahn, Yoo-Jin
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Fluid dynamics ; Volume 1 of 3 (2023)

INVESTIGA TION OF FLOW-STRUCTURE COUPLING FOR A COMPLIANT PANEL UNDER A SHOCK/BOUNDARY-LA YER INTERACTION USING FAST-RESPONSE PSP

von Musta, Mustafa N.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Applied aerodynamics ; Volume 4 of 4 (2021)

INVESTIGATION OF FLOW-STRUCTURE COUPLING FOR A COMPLIANT PANEL UNDER A SHOCK/BOUNDARY-LAYER INTERACTION USING FAST-RESPONSE PSP

von Musta, Mustafa N.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Applied aerodynamics ; Volume 3 of 4 (2021)

EFFECT OF SHOCK-WAVE BOUNDARY LAYER INTERACTION ON VIBRATORY RESPONSE OF COMPLIANT PANEL

von Eitner, Mare A.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Applied aerodynamics ; Volume 1 of 4 (2021)