Blade tips
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The concept Blade tips represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Blade tips
Resource Information
The concept Blade tips represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Blade tips
- Source
- nasat
24 Items that share the Concept Blade tips
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- Wake geometry measurements and analytical calculations on a small-scale rotor model
- A reduced model for prediction of thermal and rotational effects on turbine tip clearance
- Aerodynamic limitations of the UH-60A rotor
- Analysis of gas turbine rotor blade tip and shroud heat transfer
- Blade tip rubbing stress prediction : final report
- Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating
- 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 14- x 22-foot subsonic tunnel
- Deterministic stress modeling of hot gas segregation in a turbine
- Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines
- Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines
- Evaluation of an active clearance control system concept
- Heat transfer and flow on the first stage blade tip of a power generation gas turbine
- Heat transfer and flow on the first stage blade tip of a power generation gas turbine, Part 2, Simulation results
- Helicopter blade tips
- Integrated turbine tip clearance and gas turbine engine simulation
- Investigation of a Moiré based crack detection technique for propulsion health monitoring
- Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984
- Optical strain and crack-detection measurements on a rotating disk
- Prediction of unshrouded rotor blade tip heat transfer : under cooperative agreement NCC3-370
- Testing of a Microwave blade tip clearance sensor at the NASA Glenn Research Center
- The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor
- The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction : final technical report ...
- The three dimensional flow field at the exit of an axial-flow turbine rotor
- Toward understanding tip leakage flows in small compressor cores including stator leakage flow
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/bbC_0P_SZvo/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/bbC_0P_SZvo/">Blade tips</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/bbC_0P_SZvo/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/bbC_0P_SZvo/">Blade tips</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
