Hyplane: a single-stage suborbital aerospaceplane. [PDF]
Russo G, Voto C.
europepmc +1 more source
Thermal-Fluid-Solid Coupling-Parametrical Numerical Analysis of Hot Turbine Nozzle Guide Vane. [PDF]
Froissart M, Ochrymiuk T.
europepmc +1 more source
Analytical investigation of off-design performance of a transonic turbine [PDF]
The off-design performance and a breakdown of the losses of a transonic turbine were determined by an analytical method that was previously developed for turbines of more conservative design. The analytically obtained performance map is compared with the
Whitney, Warren J, Stewart, Warner L
core
Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]
Islam A, Ma H.
europepmc +1 more source
VAWT with controlled blades : influence of wake of one turbine on power coefficient on the next turbine [PDF]
Power production from wind turbines is affected by several conditions like wind speed, turbine speed, turbine design, turbulence, changes of wind direct ion, wake of previous turbines.
SIMONET, Sophie +2 more
core
Axial compressor blades tip leakage flow control using natural aspiration. [PDF]
Nejad PG, Zenouz RT.
europepmc +1 more source
Experimental and Computational Investigation of an “Open” Transonic Cavity Flow [PDF]
This paper presents an investigation of a transonic flow (M∞ = 0.85) over a rectangular cavity having a length-to-depth ratio of 5. Velocities were measured inside the cavity on the central plane and two off-centre planes using a two-component particle ...
Knowles, Kevin +3 more
core
AERODYNAMIC RESEARCH ON THE MIDSECTION OF A LONG TURBINE BLADE
The paper is concerned with experimental aerodynamic research on the midsection of a 1220 mm long turbine rotor blade. Optical as well as pneumatic measurements of the midsection blade cascade have been performed in a suction type high-speed wind tunnel.
DAVID SIMURDA +3 more
doaj
Effects of Double-Side Labyrinth Seals on Aerodynamic Performance in a Transonic Shrouded Turbine Stage. [PDF]
Li W, Chen S, Liu H, Zhou Z, Wang S.
europepmc +1 more source
Skin-Friction-Based Identification of the Critical Lines in a Transonic, High Reynolds Number Flow via Temperature-Sensitive Paint. [PDF]
Costantini M +3 more
europepmc +1 more source

