Online Books by
Propulsion Laboratory (U.S.)
Books from the extended shelves:
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Propulsion Laboratory (U.S.): Analysis of metal temperature and coolant flow with a thermal-barrier coating on a full-coverage-film-cooled turbine vane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Peter L. Meitner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)- Propulsion Laboratory (U.S.): Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard J. Roelke, Jeffrey E. Haas, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Comparison of predicted and measured elastohydrodynamic film thickness in a 20-millimeter-bore ball bearing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by John J. Coy, Dennis P. Townsend, Rama S. R. Gorla, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by David Rosenbaum, Lewis Research Center, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Correlation of asperity contact-time fraction with elastohydrodynamic film thickness in a 20-millimetr-bore ball bearing (National Aeronautics and Space Administration :, 1979), also by John J. Coy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Direct integration of transient rotor dynamics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Albert F. Kascack and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Effect of geometry on hydrodynamic film thickness (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by D. E. Brewe, Christopher M. Taylor, Bernard J. Hamrock, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, University of Leeds, and Lewis Research Center (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by David B. Ercegovic and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Effects of geometric variables on rub characteristics of Ti-6A1-4V (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Robert C. Bill, Donald W. Wisander, Jan Wolak, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Kerry L. McLallin, Jeffrey E. Haas, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): FORTRAN program for calculating coolant flow and metal temperatures of a full-coverage-film-cooled vane or blade (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Peter L. Meitner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Gas turbine ceramic-coated-vane concept with convection-cooled porus metal core (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Albert F. Kascak, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): High-temperature erosion of plasma-sprayed, yttria-stabilized zirconia in a simulated turbine environment (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Robert F. Handschuh, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Life analysis of multiroller planetary traction drive (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by John J. Coy, Stuart H. Loewenthal, Douglas A. Rohn, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Long-term hot-hardness characteristics of five through-hardened bearing steel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Neil E. Anderson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Multiroller traction drive speed reducer : evaluation for automotive gas turbine engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Douglas A. Rohn, Neil E. Anderson, Stuart H. Loewenthal, Army Research and Technology Laboratories (U.S.), United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Off-design performance loss model for radial turbines with pivoting, variable-area stators (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Peter L. Meitner, Arthur J. Glassman, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Donald C. Urasek, Walter S. Cunnan, William T. Gorrell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Performance of two-stage fan with a first-state rotor redesigned to account for the presence of a part-span damper (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William T. Gorrell, Donald C. Urasek, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1981), also by Jeffrey E. Haas, Paul Hermann, Richard J. Roelke, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Spur-gear-system efficiency at part and full load (National Aeronautics and Space Administration, Scientific and technical Information Office, 1980), also by Neil E. Anderson, Stuart H. Loewenthal, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Propulsion Laboratory (U.S.): Thermal stress analysis of ceramic gas-path seal components for aircraft turbines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Francis E. Kennedy, Robert C. Bill, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
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