Axial compressor blades tip leakage flow control using natural aspiration. [PDF]
Nejad PG, Zenouz RT.
europepmc +1 more source
Investigation of the three-dimensional flow field within a transonic fan rotor: Experiment and analysis [PDF]
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.
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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
Aeronautical Engineering: A special bibliography with indexes, supplement 48 [PDF]
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
Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5 [PDF]
Wind tunnel testing of thermal and pressure in base of Saturn S-IC ...
Wasko, R. A.
core +1 more source
Aeronautical Engineering: A continuing bibliography with indexes, supplement 99 [PDF]
This bibliography lists 292 reports, articles, and other documents introduced into the NASA scientific and technical information system in July ...
core +1 more source
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
Simulation of turbomachinery flows [PDF]
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.
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Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions [PDF]
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.
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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
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