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Modeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion

Title

Modeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion

Call Number

AVAILABLE ONLINE

Author

Veres, Joseph P., author. Jorgenson, Philip C. E. (Philip Charles Eberhardt), author. Jones, Scott M., author. NASA Glenn Research Center, issuing body. United States. National Aeronautics and Space Administration, sponsoring body.

Publication Information

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/gpo57061

Subsequent Title values, for Searching

Modeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion NASA/TM ; NASA technical memorandum ;

Series Title

NASA technical memorandum ;

Available:

SD_UNO:3042882

Electronic Resources

Modeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion

2014

Veres, Joseph P., author.

High-temperature, oxidation-rersistant thruster research

Title

High-temperature, oxidation-rersistant thruster research

Call Number

NAS 1.26:185233

Author

Wooten, J. R. Lansaw, P. T. Aerojet TechSystems Company (U.S.) Lewis Research Center.

Publication Information

Sacramento, Calif. : Aerojet Propulsion Division, Research & Technology ; Cleveland, Ohio : National Aeronautics & Space Administration, Lewis Research Center, [1990]

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS69660

Subsequent Title values, for Searching

High-temperature, oxidation-rersistant thruster research High temperature, oxidation resistant thruster research NASA CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:1521820

Microform

High-temperature, oxidation-rersistant thruster research

1990

Wooten, J. R.

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Cover image for Orbital transfer vehicle oxygen turbopump technology. Volume I. Design, fabrication, and hydrostatic bearing testing : final report

Orbital transfer vehicle oxygen turbopump technology. Volume I. Design, fabrication, and hydrostatic bearing testing : final report

Title

Orbital transfer vehicle oxygen turbopump technology. Volume I. Design, fabrication, and hydrostatic bearing testing : final report

Call Number

NAS 1.26:185175

Author

Buckmann, P. S. United States. National Aeronautics and Space Administration. Lewis Research Center.

Publication Information

[Washington, D.C.] : National Aeronautics and Space Administration, [1990]

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS60999

Subsequent Title values, for Searching

Orbital transfer vehicle oxygen turbopump technology. Volume I. Design, fabrication, and hydrostatic bearing testing : final report NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:1295784

Microform

Orbital transfer vehicle oxygen turbopump technology. Volume I. Design, fabrication, and hydrostatic bearing testing : final report

1990

Buckmann, P. S.

QM-8 final performance evaluation report. Volume 4. Seals

Title

QM-8 final performance evaluation report. Volume 4. Seals

Call Number

NAS 1.26:183958

Author

Nelsen, Lowell V. Thiokol Corporation. Space Operations. George C. Marshall Space Flight Center.

Publication Information

Brigham City, UT : Thiokol Corp., Space Operations ; Marshall Space Flighjt Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1989]

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS70075

Subsequent Title values, for Searching

QM-8 final performance evaluation report. Volume 4. Seals QM 8 fiinal performance evaluation report Seals NASA CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:1521955

Microform

QM-8 final performance evaluation report. Volume 4. Seals

1989

Nelsen, Lowell V.

Initial characterization of a modular heat exchanger with an integral heat pipe

Title

Initial characterization of a modular heat exchanger with an integral heat pipe

Call Number

AVAILABLE ONLINE

Author

Schreiber, Jeffrey G. United States. National Aeronautics and Space Administration.

Publication Information

[Washington, D.C.] : National Aeronautics and Space Administration, [1989]

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS107740

Subsequent Title values, for Searching

Initial characterization of a modular heat exchanger with an integral heat pipe NASA technical memorandum ;

Series Title

NASA technical memorandum ;

Available:

SD_UNO:2117257

Electronic Resources

Initial characterization of a modular heat exchanger with an integral heat pipe

1989

Schreiber, Jeffrey G.

Initial characterization of a modular heat exchanger with an integral heat pipe

Title

Initial characterization of a modular heat exchanger with an integral heat pipe

Call Number

NAS 1.15:102097

Author

Schreiber, Jeffrey G. United States. National Aeronautics and Space Administration.

Publication Information

[Washington, D.C.] : National Aeronautics and Space Administration, [1989]

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS107740

Subsequent Title values, for Searching

Initial characterization of a modular heat exchanger with an integral heat pipe NASA technical memorandum ;

Series Title

NASA technical memorandum ;

Available:

SD_UNO:2117256

Microform

Initial characterization of a modular heat exchanger with an integral heat pipe

1989

Schreiber, Jeffrey G.

SSME technology test bed fast shutdown assessment final report

Title

SSME technology test bed fast shutdown assessment final report

Call Number

NAS 1.26:179354

Author

Liebman, A. Vilja, J. O. Rockwell International. Rocketdyne Division. United States. National Aeronautics and Space Administration.

Publication Information

Canoga Park, Calif. : Rockwell International, Rocketdyne Division ; [Washington, D.C. : National Aeronautics and Space Administration, 1988]

Subsequent Title values, for Searching

SSME technology test bed fast shutdown assessment final report NASA CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:2168779

Rockwell International, Rocketdyne Division ; National Aeronautics and Space Administration,

Microform

SSME technology test bed fast shutdown assessment final report

1988

Liebman, A.

SSME seal test program : test results for hole-pattern damper seals, interim progress report

Title

SSME seal test program : test results for hole-pattern damper seals, interim progress report

Call Number

AVAILABLE ONLINE

Author

Childs, Dara W. author. United States. National Aeronautics and Space Administration, issuing body. Texas A & M University. Turbomachinery Laboratories.

Publication Information

[Washington, D.C.] : [National Aeronautics and Space Administration], July 1985.

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/gpo107989

Subsequent Title values, for Searching

SSME seal test program : test results for hole-pattern damper seals, interim progress report Test results for hole-pattern damper seals NASA/CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:3617030

Electronic Resources

SSME seal test program : test results for hole-pattern damper seals, interim progress report

1985

Childs, Dara W. author.

Energy efficient engine high pressure turbine component rig performance test report

Title

Energy efficient engine high pressure turbine component rig performance test report

Call Number

AVAILABLE ONLINE

Author

Leach, K. P., author. Lewis Research Center, issuing body. United Technologies Corporation.

Publication Information

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1983.

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/gpo93106

Subsequent Title values, for Searching

Energy efficient engine high pressure turbine component rig performance test report NASA/CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:3602592

Electronic Resources

Energy efficient engine high pressure turbine component rig performance test report

1983

Leach, K. P., author.

10.

Baseline testing of the EV Global E-Bike

Title

Baseline testing of the EV Global E-Bike

Call Number

AVAILABLE ONLINE

Author

Eichenberg, Dennis J., author. Kolacz, John S., author. Tavernelli, Paul F., author. NASA Glenn Research Center, issuing body.

Publication Information

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2001.

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/LPS26737

Subsequent Title values, for Searching

Baseline testing of the EV Global E-Bike NASA/TM ; NASA technical memorandum ;

Series Title

NASA technical memorandum ;

Available:

SD_UNO:3576617

Electronic Resources

Baseline testing of the EV Global E-Bike

2001

Eichenberg, Dennis J., author.

11.

Baseline testing of the EV Global E-Bike

Title

Baseline testing of the EV Global E-Bike

Call Number

NAS 1.15:210569

Author

Eichenberg, Dennis J. Kolacz, John S. Tavernelli, Paul F. NASA Glenn Research Center.

Publication Information

[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]

Subsequent Title values, for Searching

Baseline testing of the EV Global E-Bike [NASA technical memorandum] ; NASA technical memorandum ;

Series Title

NASA technical memorandum ;

Available:

SD_UNO:908190

Microform

Baseline testing of the EV Global E-Bike

2001

Eichenberg, Dennis J.

12.

High pressure turbine ceramic shroud support technology report

Title

High pressure turbine ceramic shroud support technology report

Call Number

AVAILABLE ONLINE

Author

Nelson, W. A., author. Carlson, R. G., author. Lewis Research Center, issuing body.

Publication Information

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1982.

Electronic Access

http://utils.louislibraries.org/cgi-bin/lz0050.x?sitecode=LANO?https://purl.fdlp.gov/GPO/gpo107828

Subsequent Title values, for Searching

High pressure turbine ceramic shroud support technology report Energy efficient engine NASA/CR ; NASA contractor report ;

Series Title

NASA contractor report ;

Available:

SD_UNO:3616959

Electronic Resources

High pressure turbine ceramic shroud support technology report

1982

Nelson, W. A., author.

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Author

United States. National Aeronautics and Space Administration.

(19)

Lewis Research Center.

(13)

Lewis Research Center, issuing body.

(8)

NASA Glenn Research Center.

(8)

NASA Glenn Research Center, issuing body.

(4)

United States. Department of Energy. Office of Vehicle and Engine Research and Development

(3)

Browning, L.

(2)

DeLaat, John C.

(2)

Dryden Flight Research Facility.

(2)

General Motors Corporation. Allison Gas Turbine Division.

(2)

George C. Marshall Space Flight Center.

(2)

Hultgren, Lennart S. (Lennart Sven)

(2)

Humbert, D. R.

(2)

Merrill, Walter C.

(2)

Miles, Jeffrey H. (Jeffrey Hilton)

(2)

Millan, P. P.

(2)

Pefley, Richard K.

(2)

Perkins, H. Douglas, author.

(2)

Perkins, H. Douglas.

(2)

Schreiber, Jeffrey G.

(2)

Texas A & M University. Turbomachinery Laboratories.

(2)

Thomas, Scott R.

(2)

Thomas, Scott R., author.

(2)

U.S. Army Research Laboratory.

(2)

United States. National Aeronautics and Space Administration, sponsoring body.

(2)

AIAA Aeroacoustics Conference (30th : 2009 : Miami, Fla.)

(1)

AIAA Aerospace Sciences Meeting (48th : 2010 : Orlando, Fla.)

(1)

AIAA Guidance, Navigation, and Control Conference (2011 : Portland, Or.)

(1)

AIAA/CEAS Aeroacoustics Conference (15th : 2009 : Miami, Fla.)

(1)

AIAA/CEAS Aeroacoustics Conference (17th : 2011 : Portland, Or.)

(1)

ASME Turbo Expo (2010 : Glasgow, Scotland)

(1)

Acosta, Waldo A.

(1)

Acosta, Waldo A., author.

(1)

Aerojet TechSystems Company (U.S.)

(1)

Akkerman, J. W.

(1)

Allied-Signal Aerospace Company. Garrett Auxiliary Power Division.

(1)

American Institute of Aeronautics and Astronautics.

(1)

Arora, Gul K.

(1)

Arora, Gul K., author.

(1)

Beitler, R. S., author.

(1)

Biaglow, James A.

(1)

Bridges, James E., 1943-

(1)

Buckmann, P. S.

(1)

Burcham, Frank W.

(1)

Carlson, R. G., author.

(1)

Chamis, C. C. (Christos C.)

(1)

Childs, Dara W.

(1)

Childs, Dara W. author.

(1)

Cramer, J. M.

(1)

Eichenberg, Dennis J.

(1)

Eichenberg, Dennis J., author.

(1)

Fazah, M. M.

(1)

Fazah, M. M., author.

(1)

Flegel, Ashlie B., author.

(1)

General Electric Company.

(1)

George C. Marshall Space Flight Center, issuing body.

(1)

Henderson, Brenda S.

(1)

Howard, Samuel A., active 1850-1857, author.

(1)

Jassowski, D. M.

(1)

Johns, Robert H.

(1)

Johnson, J. Blair.

(1)

Johnson, Susan M. (Susan Margaret), 1952-

(1)

Joint Propulsion Conference and Exhibit (46th : 2010 : Nashville, Tenn.)

(1)

Jones, Scott M., author.

(1)

Jorgenson, Philip C. E. (Philip Charles Eberhardt), author.

(1)

Kolacz, John S.

(1)

Kolacz, John S., author.

(1)

Lansaw, P. T.

(1)

Lavash, J. P., author.

(1)

Leach, K. P., author.

(1)

Lepicovsky, Jan, author.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Mechanical Technology Incorporated.

(1)

(1)

(1)

(1)

(1)

Nelson, W. A., author.

(1)

Oliver, Michael J., author.

(1)

Owen, A. Karl, author.

(1)

Owen, A. Karl.

(1)

Pack, William D.

(1)

Pack, William D., author.

(1)

Podboy, Gary G.

(1)

Pollard, James E.

(1)

Proctor, Margaret P.

(1)

Proctor, Margaret P., author.

(1)

Rockwell International. Rocketdyne Division.

(1)

Shah, Ashwin.

(1)

Smith, John M.

(1)

Tavernelli, Paul F.

(1)

Tavernelli, Paul F., author.

(1)

Thiokol Corporation. Space Operations.

(1)

Tomazic, William A.

(1)

Trefny, Charles J.

(1)

Trefny, Charles J., author.

(1)

U.S. Army Research Laboratory, sponsoring body.

(1)

United States. Department of Energy. Heat Engine Propulsion Division.

(1)

United States. Department of Energy. Office of Transportation Systems

(1)

United States. Department of Energy. Office of Transportation Technologies.

(1)

United States. Department of Energy. Office of Vehicle and Engine Research and Development.

(1)

United States. National Aeronautics and Space Administration, issuing body.

(1)

United Technologies Corporation.

(1)

Veres, Joseph P., author.

(1)

(1)

(1)

(1)

Subject

(57)

(6)

(6)

(6)

(5)

Propulsion system performance.

(5)

(4)

(4)

(4)

(4)

(4)

Airplanes -- Control systems.

(3)

Centrifugal force.

(3)

Ceramics.

(3)

Compressors.

(3)

Computerized simulation.

(3)

(3)

(3)

(3)

(3)

(3)

Oxidation resistance.

(3)

Protective coatings.

(3)

Space Shuttle Main Engine.

(3)

(3)

(3)

(3)

(2)

(2)

(2)

Airplanes -- Motors -- Starting devices.

(2)

(2)

(2)

(2)

(2)

Automotive gas turbines.

(2)

Axial loads.

(2)

Brush seals.

(2)

Centrifugal compressors.

(2)

(2)

(2)

(2)

(2)

(2)

(2)

(2)

(2)

Electric equipment tests.

(2)

(2)

(2)

(2)

(2)

Feasibility analysis.

(2)

Firing (igniting)

(2)

Flow characteristics.

(2)

(2)

(2)

(2)

(2)

(2)

(2)

Gas-gas interactions.

(2)

(2)

(2)

(2)

(2)

(2)

(2)

Hypersonic wind tunnels.

(2)

Ice formation.

(2)

Injectors.

(2)

Integral rocket ramjets.

(2)

(2)

(2)

(2)

(2)

Oxide dispersion strengthening.

(2)

Paints.

(2)

Photochemical reactions.

(2)

Pressure measurement.

(2)

Propellant combustion.

(2)

Propulsion system configurations.

(2)

(2)

(2)

(2)

(2)

(2)

(2)

(2)

(2)

(2)

Supersonic transports.

(2)

TU-144 aircraft.

(2)

Temperature measurement.

(2)

Thermal analysis.

(2)

Thermocouples.

(2)

Thrust.

(2)

Tube heat exchangers.

(2)

Turbine blades.

(2)

Turbojet engine control.

(2)

Turboshafts.

(2)

Wear.

(2)

Wind tunnel tests.

(2)

Acceleration (physics)

(1)

Acoustics.

(1)

Aerodynamic configurations.

(1)

Aerodynamics, Supersonic.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Airplanes -- Ramjet engines.

(1)

Airplanes -- Scramjet engines.

(1)

Altitude simulation.

(1)

Altitude tests.

(1)

Automatic diagnostics.

(1)

Beam currents.

(1)

Bird-aircraft collisions.

(1)

Charged particles.

(1)

Combustion efficiency.

(1)

Combustion.

(1)

Communication satellites.

(1)

Component reliability.

(1)

Computer programming.

(1)

Computer systems programs.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Distributed processing.

(1)

Engine -- Examinations.

(1)

Engine control.

(1)

Engine monitoring instruments.

(1)

Engines -- Examinations.

(1)

External tanks.

(1)

F-15 aircraft.

(1)

Fighter planes -- Flight testing.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Gas-turbines -- Combustion chambers.

(1)

Heat transfer.

(1)

High altitude.

(1)

High pressure oxygen.

(1)

High temperature research.

(1)

Holes (mechanics)

(1)

Hydrogen.

(1)

Hypersonic planes.

(1)

Hypervelocity impact.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Jet planes -- Thrust reversers.

(1)

Lateral control.

(1)

Life (durability)

(1)

Liquid oxygen.

(1)

Liquid propellant rocket engines.

(1)

Liquid rocket propellants.

(1)

Mechanical engineering.

(1)

Nitrogen tetroxide.

(1)

Noise measurement.

(1)

Noise prediction.

(1)

Orbit transfer vehicles.

(1)

(1)

(1)

(1)

(1)

(1)

(1)

(1)

Pressure -- Measurement.

(1)

Pressure effects.

(1)

Propellants.

(1)

Propulsion.

(1)

Propulsive efficiency.

(1)

Qualifications.

(1)

Research and development.

(1)

Rocket engine design.

(1)

(1)

(1)

(1)

(1)

Software engineering.

(1)

Sound generators.

(1)

Space Shuttle Boosters.

(1)

Spacecraft propulsion.

(1)

(1)

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