Books on the topic '"turbine blade tip rub"'
Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles
Consult the top 20 books for your research on the topic '"turbine blade tip rub".'
Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.
You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.
Browse books on a wide variety of disciplines and organise your bibliography correctly.
A, Davis Gary. Blade tip rubbing stress prediction: Final report. Rockwell International, Rocketdyne Division, 1991.
Find full textAmeri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. National Aeronautics and Space Administration, 1996.
Find full textAmeri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. National Aeronautics and Space Administration, 1998.
Find full textMartinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.
Find full textMartinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.
Find full textYamamoto, Atsumasa. Mechanisms of endwall/leakage flows and the associated losses in a linear turbine rotor cascade with blade tip-clearance. National Aerospace Laboratory, 1988.
Find full textKypuros, Javier A. A reduced model for prediction of thermal and rotational effects on turbine tip clearance. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Find full textMartinez-Sanchez, Manuel. Phase III report on contract number NAS8-35018 entitled Turbine blade tip and seal clearance excitation forces. National Aeronautics and Space Administration, 1992.
Find full textLattime, Scott B. Turbine engine clearance control systems: Current practices and future directions. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textT, Arts, and Von Karman Institute for Fluid Dynamics., eds. Turbine blade tip design and tip clearance treatment: January 19-23, 2003. Von Karman Institute for Fluid Dynamics, 2004.
Find full textM, Savino J., and United States. Dept. of Energy. Wind Energy Technology Division., eds. Reflection plane tests of a wind turbine blade tip section with ailerons. U.S. Dept. of Energy, Wind Energy Technology Division, 1985.
Find full textM, Greitzer Edward, George C. Marshall Space Flight Center., and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.
Find full textM, Greitzer Edward, George C. Marshall Space Flight Center, and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.
Find full textE, Steinthorsson, and United States. National Aeronautics and Space Administration., eds. Prediction of unshrouded rotor blade tip heat transfer: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1994.
Find full textL, Rigby D., and NASA Glenn Research Center, eds. A numerical analysis of heat transfer and effectiveness on film cooled turbine blade tip models. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textHeat transfer and flow on the first stage blade tip of a power generation gas turbine. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textJ, Melcher Kevin, and NASA Glenn Research Center, eds. A reduced model for prediction of thermal and rotational effects on turbine tip clearance. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Find full textCenter, NASA Glenn Research, ed. Heat transfer and flow on the blade tip of a gas turbine equipped with a mean-camberline strip. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textTurbine engine clearance control systems: Current practices and future directions. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textUnited States. National Aeronautics and Space Administration., ed. HEAT TRANSFER AND FLOW ON THE BLADE TIP OF A GAS TURBINE EQUIPPED WITH A MEAN-CAMBERLINE STRIP FINAL REPORT... NASA/CR-2001-210764... AUG. s.n., 2002.
Find full text