Turbine engines
Resource Information
The concept Turbine engines represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
The Resource
Turbine engines
Resource Information
The concept Turbine engines represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
- Label
- Turbine engines
- Source
- nasat
48 Items that share the Concept Turbine engines
Context
Context of Turbine enginesSubject of
No resources found
No enriched resources found
- U.S. civil rotorcraft accidents, 1963 through 1997
- 2004 NASA Seal/Secondary Air System workshop : proceedings of a conference held at Ohio Aerospace Institute sponsored by NASA Glenn Research Center, Cleveland, Ohio November 9-10, 2004
- A new method to measure temperature and burner pattern factor sensing for active engine control
- A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool
- Advanced Turbine Technology Applications Project (ATTAP : 1988 annual report
- Advanced seal technology role in meeting next generation turbine engine goals
- Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model
- Aircraft turbine engine control research at NASA Glenn Research Center
- Computational analyses of the LIMX TBCC inlet high-speed flowpath
- Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research
- Damage tolerance and reliability of turbine engine components
- Deformation mechanisms of NiAl cyclicly deformed near the brittle-to-ductile transition temperature : final report
- Design, installation, and evaluation of an altitude test facility modification
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Dynamic systems analysis for turbine based aero propulsion systems
- Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments
- Experimental and analytical study of ceramic-coated turbine-tip shroud seals for small turbine engines
- Four spot laser anemometer and optical access techniques for turbine applications
- Full-scale thrust reverser testing in an altitude facility
- HPT clearance control : intelligent engine systems : phase 1
- Health monitoring of a rotating disk using a combined analytical-experimental approach
- High Stability Engine Control (HISTEC) : flight demonstration results
- High pressure angle gears : preliminary testing results
- High stability engine control (HISTEC) : flight demonstration results
- Improving data collection and analysis interface for the data acquisition software of the spin laboratory at NASA Glenn Research Center
- Integrated tools for future distributed engine control technologies
- Model-based fault diagnosis for turboshaft engines
- Modern experimental techniques in turbine engine testing
- Modern experimental techniques in turbine engine testing
- NASA aeropropulsion research
- Neural network-based sensor validation for turboshaft engines
- Off-design performance loss model for radial turbines with pivoting, variable-area stators
- Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile
- Preliminary design of a supersonic cruise aircraft high-pressure turbine : final report
- Preliminary tuft testing of metallic bristles versus PS212, PS300, and HVOF300
- Pressure balanced, low hysteresis, finger seal test results
- Propulsion health monitoring of a turbine engine disk using spin test data
- Revisiting the birth of 7YSZ thermal barrier coatings : Steve Stecura
- Shock position control for mode transition in a turbine based combined cycle engine inlet model
- SiC and Si[subscript 3]N[subscript 4] recession due to SiO[subscript 2] scale volatility under combustor conditions
- Simulation of turbine tone noise generation using a turbomachinery aerodynamics solver
- Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines
- Testing of the NASA Hypersonics project's Combined Cycle Engine Large Scale Inlet Mode Transition Experiment (CCE LIMX)
- Tool for the integrated dynamic numerical propulsion system simulation (NPSS)/turbine engine closed-loop transient analysis (TTECTrA) : user's guide
- Tool for turbine engine closed-loop transient analysis (TTECTrA) users' guide
- Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils
- U.S. civil rotorcraft accidents, 1963 through 1997
Embed
Settings
Select options that apply then copy and paste the RDF/HTML data fragment to include in your application
Embed this data in a secure (HTTPS) page:
Layout options:
Include data citation:
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/m8ECxsz6-xM/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/m8ECxsz6-xM/">Turbine engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements
Preview
Cite Data - Experimental
Data Citation of the Concept Turbine engines
Copy and paste the following RDF/HTML data fragment to cite this resource
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/m8ECxsz6-xM/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/m8ECxsz6-xM/">Turbine engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
