Airplanes -- Turbojet engines
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The concept Airplanes -- Turbojet engines represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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Airplanes -- Turbojet engines
Resource Information
The concept Airplanes -- Turbojet engines represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Airplanes -- Turbojet engines
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- (EG-IN)1255343
46 Items that share the Concept Airplanes -- Turbojet engines
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- What every member of the trade community should know about : turbojets, turbopropellers and other gas turbines, (HTSUS 8411) and parts thereof
- Adiabatic Wankel type rotary engine
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet
- Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle
- Ambient temperature and humidity correction factors for exhaust emissions from two classes of aircraft turbine engines
- Analysis of a topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel
- Analytical study of mixed-flow JT8D exhaust emissions measurements for fixed-probe requirements
- Behavior of turbulent gas jets in an axisymmetric confinement
- Comparison of calculated and altitude-facility-measured thrust and airflow of two prototype F100 turbofan engines
- Conceptual study of a turbojet/ramjet inlet
- Development, acquisition, and operating and support cost methods for aircraft turbine engines
- Effect of flame stabilizer design on performance and exhaust pollutants of a two-row swirl-can combustor operated to near-stoichiometric conditions
- Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles
- Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment
- Energy efficient engine : flight propulsion system preliminary analysis and design update
- Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility
- F-15 and F-16 engine problems : hearing before the Committee on Armed Services, United States Senate, Ninety-sixth Congress, first session, November 27, 1979
- Flight engineer : turbojet-basic written test guide
- Flow field survey near the rotational plane of an advanced design propeller on a Jetstar airplane
- Fluid machines : expanding the limits, past and future
- Gas turbines for aircraft
- High frequency-heated air turbojet
- Jet propulsion turbojets
- Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics
- Measurement uncertaintyfor the uniform engine testing program conducted at the NASA Lewis Research Center
- Method and system for monitoring and displaying engine performance parameters : patent application
- NASTRAN documentation for flutter analysis of advanced turbopropellers
- Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5
- Performance potential of an advanced technology Mach 3 turbojet engine installed on a conceptual high-speed civil transport
- Perspectives on dilution jet mixing
- Plotting component maps in the Navy/NASA Engine Program (NNEP) : a method and its usage
- Skyrocketing into the unknown
- Small gas turbine combustor experimental study : complaint metal/ceramic liner and performance evaluation
- Small, low-cost, expendable turbojet engine : I - design, fabrication, and preliminary testing
- Small, low-cost, expendable turbojet engine : II - performance characteristics
- Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor
- Study of effects of fuel properties in turbine-powered business aircraft : final report
- Study to improve turbine engine roto blade containment / K. F. Heerman, K. R. McClure, R. H. Eriksson
- The US Army Transportation School Apprenticeship Program for the trade of aircraft engine mechanic (turbine)
- The future challenge for aeropropulsion
- Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
- Turbine engine particulate emission characterization
- Turbine engine particulate emission characterization
- Turbine engine particulate emission characterization
- Turbojet fundamentals
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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.library.in.gov/resource/ogdSCI13770/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/ogdSCI13770/">Airplanes -- Turbojet engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</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.library.in.gov/resource/ogdSCI13770/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/ogdSCI13770/">Airplanes -- Turbojet engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
