Experimental investigation of the supersonic cavity by spectral-POD of high-sampling rate pressure-sensitive paint data

Y Oka, Y Ozawa, T Nagata, K Asai, T Nonomura - Experiments in Fluids, 2023 - Springer
A pressure distribution inside a two-dimensional rectangular cavity with a ratio L/D= 5.0 of
the cavity length L to the depth D over a supersonic flow was obtained using an improved …

Three-dimensional flow structures and heat transfer characteristics of compressible flow over a cylindrical cavity

J Wang, T Ma, Z Wang, R Wang, H Song… - Aerospace Science and …, 2022 - Elsevier
High-speed flows over a cavity produce remarkably local heat augments. Heat transfer
characteristics of compressible flow over a cylindrical cavity were revealed using wind …

[HTML][HTML] Low-frequency, spanwise oscillation in a finite-width cavity at Mach 1.5

AM Turpin, RL Speth, SE Sherer, KO Granlund - Physics of Fluids, 2021 - pubs.aip.org
A joint experimental–computational program examined low-frequency, spanwise oscillations
in supersonic flow over a finite-width cavity. Lowpass-filtered rear wall surface pressure …

Stable dynamic mode decomposition algorithm for noisy pressure-sensitive-paint measurement data

Y Ohmichi, Y Sugioka, K Nakakita - AIAA Journal, 2022 - arc.aiaa.org
AN INCREASING number of large-scale time-series datasets are being generated with the
development of numerical and experimental techniques. For example, pressure-sensitive …

Supersonic cavity flow subjected to continuous and transient leading-edge blowing

AM Turpin, D Chin, K Granlund - AIAA Journal, 2020 - arc.aiaa.org
A rectangular cavity (L/D= 5.67) with Mach 1.5 freestream was subjected to a large temporal
variation in leading-edge blowing in order to experimentally investigate the effect on …

Measurements of a Mach 3.4 turbulent boundary layer using stereoscopic particle image velocimetry

RB Panco, EP DeMauro - Experiments in Fluids, 2020 - Springer
Experiments were performed within the Rutgers University Mach 3.4 supersonic wind tunnel
to quantify the turbulent boundary layer in the test section, using stereoscopic particle image …

[HTML][HTML] Detached Eddy Simulations of Cavity-Store Interactions at Subsonic Turbulent Flow

H Ben-Gida - Aerospace, 2023 - mdpi.com
Weapons bays have gained much attraction in the last decade, mainly in the context of next-
generation aircraft. Although internal store carriage provides numerous advantages, aero …

Experimental study of an air-to-ground store release from a jet-fighter weapons bay in Transonic flow conditions

H Ben-Gida - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-4497. vid In this study, wind tunnel
experiments are conducted to study the release of an air-to-ground store (AGS) model from …

Experimental investigation of vortex breakdown in oblique shock-vortex interactions

J Thompson, RM Kiriakos, EP DeMauro - AIAA AVIATION 2021 FORUM, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-2850. vid Stereoscopic particle
image velocimetry experiments were conducted within the Rutgers University Mach 3.4 …

[图书][B] Time-Dependent Aerodynamic Loads on Store in/near Supersonic Cavity

DY Chin - 2019 - search.proquest.com
The problem of safe store separation from a captive position in a weapons bay to a
controlled departure trajectory into transonic-and supersonic-flight speeds has been …