Mechanical & Aerospace Engineering

High-speed schlieren and 10-Hz Kr PLIF for the new AFRL mach-6 Ludwieg tube hypersonic wind tunnel

AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting.

Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration

47th AIAA Fluid Dynamics Conference, 2017.

Parametric study of forced ignition in laminar and turbulent methane jets

53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017.

Experimental investigation of shock boundary layer interactions in axisymmetric isolator geometries

53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017.

Numerical investigation of scoop effect on film cooling for cylindrical inclined hole

ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE), 8.

Numerical & experimental investigations for flow fields under non-reacting & reacting conditions through a lean premixed fuel nozzle

Proceedings of the ASME Turbo Expo, 5C-2017.

Isothermal coherent structures and turbulent flow produced by a gas turbine combustor lean pre-mixed swirl fuel nozzle

Experimental Thermal and Fluid Science, 81, 187–201.

Heat transfer enhancement by criss-cross pattern formed by 45° Angled rib turbulators in a straight square duct

ASME 2017 Heat Transfer Summer Conference, HT 2017, 1.

Heat Transfer Performance of a Transonic Turbine Blade Passage in the Presence of Leakage Flow Through Upstream Slot and Mateface Gap With Endwall Contouring

Journal of Turbomachinery, 139(12).

Film Cooling Performance of Tripod Antivortex Injection Holes Over the Pressure and Suction Surfaces of a Nozzle Guide Vane

Journal of Thermal Science and Engineering Applications, 9(2).

Experimental study of heat transfer augmentation in a two-pass channel featuring V-shaped ribs and cylindrical dimples

Applied Thermal Engineering, 116, 205–216.

Investigation of isothermal convective heat transfer in an optical combustor with a low-emissions swirl fuel nozzle

Applied Thermal Engineering, 114, 65–76.

Flow field and wall temperature measurements for reacting flow in a lean premixed swirl stabilized can combustor

Proceedings of the ASME Turbo Expo, 5C-2017.

Effect of endwall contouring on a transonic turbine blade passage: Heat transfer performance

Journal of Turbomachinery, 139(1).

A transient liquid crystal image technique for local heat transfer distributions near a sharp 180° turn of a two-pass smooth square channel

Journal of Flow Visualization and Image Processing, 24(1-4), 127–140.

Experimental investigation of rotating rib roughened two-pass square duct with two different channel orientations

Proceedings of the ASME Turbo Expo, 5A-2017.

Experimental based empirical model of the initial onset of sand deposits on hastelloy-X from 1000°C to 1100°C using particle tracking

Proceedings of the ASME Turbo Expo, 2D-2017.

Experimental and numerical investigation of heat transfer inside two-pass rib roughened duct (AR = 1:2) under rotating and stationary conditions

International Journal of Heat and Mass Transfer, 113, 384–398.

Effects of spent air removal scheme on internal-side heat transfer in an impingement-effusion system at low jet-to-target plate spacing

International Journal of Heat and Mass Transfer, 108, 998–1010.

Characterization of heat transfer enhancement and frictional losses in a two-pass square duct featuring unique combinations of rib turbulators and cylindrical dimples

International Journal of Heat and Mass Transfer, 106, 629–647.