Cover Image

Effect of cage design on characteristics of high-speed-jet-lubricated 35-millimeter-bore ball bearing/

Main Author:	Schuller, Fredrick T.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lewis Research Center
Other Authors:	Pinel, Stanley I., Signer, Hans R.
Format:	Book
Language:	English
Published:	Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:	NASA technical paper 1732
Subjects:	Airplanes > Turbojet engines > Bearings Airplanes > Turbojet engines

Similar Items

Advanced jet engine combustor test facility/
by: Adam, Paul W.
Published: (1970)

Compressor surge and stall/
by: Pampreen, Ronald C.
Published: (1993)

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41/
by: Smith, John M. 1922-
Published: (1978)

Design and performance of gas turbine power plants/
Published: (1960)

Altitude test of several afterburner configurations on a turbofan engine with a hydrogen heater to simulate an elevated turbine discharge temperature : Roy L. Johnsen and Richard R. Cullom
by: Johnsen, Roy L.
Published: (1977)

Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet/
by: Sanders, Bobby W.
Published: (1980)

Design and cold-air test of single-stage uncooled core turbine with high work output/
Published: (1980)

Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2/
by: Cubbage, James M.
Published: (1977)

A new blade element method for calculating the prformance of high and intermediate solidity axial flow fans/
by: Borst, Henry V.
Published: (1978)

Guide to in-flight thrust measurement of turbojets and fan engines/
Published: (1979)

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients/
by: Sanders, Bobby W.
Published: (1980)

Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries/
by: Hawk, J. Dennis
Published: (1979)

A method for obtaining practical flutter-suppression control laws using results of optimal control theory/
by: Newsom, Jerry R.
Published: (1979)

Operating characteristics of a high-speed, jet-lubricated 35-millimeter-bore ball bearing with a single-outer-land guided cage/
by: Schuller, Fredrick T.
Published: (1980)

Gas turbine propulsion systems
by: MacIsaac, Bernie.
Published: (2011)

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude/
by: Straight, David M.
Published: (1983)

Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics/
by: Schweikhard, William G.
Published: (1983)

Metal fatigue damage--mechanism, detection, avoidance, and repair : with special reference to gas turbine components /
Published: (1971)

Flight effects on noise generated by the JT8D-17 engine in a quiet nacelle and a conventional nacelle as measured in the NASA-Ames 40-by 80-foot wind tunnel : Summary report /
by: Strout, Frank G.
Published: (1976)

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles/
by: Head, Verlon L.
Published: (1984)

ALtitude calibration of an F100, S/N P680063, turbofan engine/
by: Biesiadny, Thomas J.
Published: (1978)

Automated procedure for developing hybrid computer simulations of turbofan engines/
by: Szuch, John R.
Published: (1982)

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel/
by: Strout, Frank G.
Published: (1978)

Flow visualization of film cooling with spanwise injection from a small array of holes and compound-angle injection from a large array/
by: Russell, Louis M.
Published: (1978)

Operating condition and geometry effects on low-frequency afterburner combustion instability in a turbofan at altitude/
by: Cullom, Richard R.
Published: (1979)

Performance of jet and inner-ring-lubricated 35-millimeter-bore ball bearings operating to 2.5 million DN/
by: Schuller, Fredrick T.
Published: (1981)

Airflow and thrust calibration of an F100 engine, S/N P680059, at selected flight conditions/
by: Biesiadny, Thomas J.
Published: (1978)

Jet propulsion : a simple guide to the aerodynamic and thermodynamic design and performance of jet engines /
by: Cumpsty, Nicholas
Published: (1997)

Turbine engine testing : papers presented at the 56th symposium of the AGARD Propulsion and Energetics Panel, held at the Jolly Ambasciatori Hotel, Turin, Italy, on 29 September-3 October 1980
Published: (1981)

Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane/
by: Kurtenbach, Frank J.
Published: (1981)

Stresses, vibrations, structural integration and engine integrity (including aeroelasticity and flutter) : copies of papers and discussions presented at the Propulsion and Energetics Panel's 52nd meeting, a symposium held in Cleveland, Ohio, USA, 23-28 October 1978
Published: (1979)

Exhaust emission calibration of two J-58 afterburning turbojet engines at simulated high-altitude, supersonic flight conditions/
by: Holdeman, James D.
Published: (1976)

Air-breathing engine test facilities register/
Published: (1981)

Aero-engine design : a state of the art : April 7-11, 2003 /
Published: (2003)

The history of aircraft gas turbine engine development in the United States .. : a tradition of excellence /
by: St. Peter, James

Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility/
by: Kurtenbach, Frank J.
Published: (1979)

Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field lenght/
by: Bowles, Jeffrey V.
Published: (1976)

Effect of two inner-ring oil-flow distribution schemes on the operating characteristics of a 35-millimeter-bore ball bearing to 2.5 million DN/
by: Schuller, Fredrick T.
Published: (1985)

A simulation evaluation of the Engine Monitoring and Control System display/
by: Abbott, Terence S.
Published: (1990)

Experimental evaluation of a mach 3.5 axisymmetric inlet/
by: Syberg, J.
Published: (1975)

Cannot write session to /tmp/vufind_sessions/sess_45n2cpbbhq6ub00m9agl1hgp14