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Blade tips
Clearances 7
Heat transfer 7
Gas turbines 6
Acoustic properties 5
Gas-turbines 5
Turbine blades 5
Aerodynamic noise 4
Axial flow turbines 4
Blade-vortex interaction 4
Computational fluid dynamics 4
Heat 4
Rotary wings 4
Rotors 4
Transmission 4
Vortices 4
Aeroacoustics 3
Aerodynamic characteristics 3
Blade slap noise 3
Flow distribution 3
Gas turbine engines 3
Helicopters 3
Mathematical models 3
Rotor aerodynamics 3
Compressor blades 2
Cracks 2
Detection 2
Euler equations of motion 2
High speed 2
Horizontal flight 2

Heat transfer and flow on the first stage blade tip of a power generation gas turbine. by Ameri, Ali A.

Analysis of gas turbine rotor blade tip and shroud heat transfer by Ameri, Ali A.

Integrated turbine tip clearance and gas turbine engine simulation / by Chapman, Jeffryes W.

Evaluation of an active clearance control system concept

Wake geometry measurements and analytical calculations on a small-scale rotor model

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 by Parzych, David J.

Evaluation of a doubly-swept blade tip for rotorcraft noise reduction by Wake, Brian E.

Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor by Suder, Kenneth L.

Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight preliminary PSP results from test 581 in the...

Ramp-integration technique for capacitance-type blade-tip clearance measurement by Sarma, Garimella R.

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating by Shyam, Vikram

Investigation of a Moiré based crack detection technique for propulsion health monitoring

Toward understanding tip leakage flows in small compressor cores including stator leakage flow / by Berdanier, Reid A., Key, Nicole L.

Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines by Ameri, Ali A.

Helicopter blade tips by Lyothier, R.

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 by Parzych, David J.

Optical strain and crack-detection measurements on a rotating disk / by Woike, Mark R.

Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades by Baeder, J. D.

The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / by Bozak, Richard F., Hughes, Christopher E., Buckley, James (Mechanical engineer)

Optical measurement of unducted fan flutter by Kurkov, Anatole P.

Search Results

Heat transfer and flow on the first stage blade tip of a power generation gas turbine. by Ameri, Ali A.

Analysis of gas turbine rotor blade tip and shroud heat transfer by Ameri, Ali A.

Integrated turbine tip clearance and gas turbine engine simulation / by Chapman, Jeffryes W.

Evaluation of an active clearance control system concept

Wake geometry measurements and analytical calculations on a small-scale rotor model

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 by Parzych, David J.

Evaluation of a doubly-swept blade tip for rotorcraft noise reduction by Wake, Brian E.

Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor by Suder, Kenneth L.

Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight preliminary PSP results from test 581 in the...

Ramp-integration technique for capacitance-type blade-tip clearance measurement by Sarma, Garimella R.

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating by Shyam, Vikram

Investigation of a Moiré based crack detection technique for propulsion health monitoring

Toward understanding tip leakage flows in small compressor cores including stator leakage flow / by Berdanier, Reid A., Key, Nicole L.

Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines by Ameri, Ali A.

Helicopter blade tips by Lyothier, R.

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 by Parzych, David J.

Optical strain and crack-detection measurements on a rotating disk / by Woike, Mark R.

Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades by Baeder, J. D.

The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / by Bozak, Richard F., Hughes, Christopher E., Buckley, James (Mechanical engineer)

Optical measurement of unducted fan flutter by Kurkov, Anatole P.

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