Results 111 to 120 of about 9,981 (232)

Investigation of the three-dimensional flow field within a transonic fan rotor: Experiment and analysis [PDF]

open access: yes
An experimental investigation of the three dimensional flow field through a low aspect ratio, transonic, axial flow fan rotor has been conducted using an advanced laser anemometer (LA) system. Laser velocimeter measurements of the rotor flow field at the
Pierzga, M. J., Wood, J. R.
core   +1 more source

Aeronautical Engineering: A special bibliography with indexes, supplement 48 [PDF]

open access: yes
This special bibliography lists 291 reports, articles, and other documents introduced into the NASA scientific and technical information system in August ...

core   +1 more source

Aeronautical Engineering: A continuing bibliography with indexes, supplement 99 [PDF]

open access: yes
This bibliography lists 292 reports, articles, and other documents introduced into the NASA scientific and technical information system in July ...

core   +1 more source

Simulation of turbomachinery flows [PDF]

open access: yes
With the interest in jet propulsion at the end of World War II, aerodynamicists were challenged to develop mathematical models which could be used to design turbomachinery components for jets.
Adamczyk, John J.
core   +1 more source

Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions [PDF]

open access: yes
A method for predicting the unsteady aerodynamic response of a cascade of airfoils to entropic, vortical, and acoustic gust excitations is being developed.
Hall, Kenneth C., Verdon, Joseph M.
core   +1 more source

AERODYNAMIC RESEARCH ON THE MIDSECTION OF A LONG TURBINE BLADE

open access: yesTASK Quarterly, 2008
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  

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