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  1. 1
    Aircraft propulsion

    Aircraft propulsion by Babu, V.

    Boca Raton, FL, U.S.A. : New Delhi, India : CRC Press ; Ane Books India, 2009
    Format: Book


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  2. 2
    Noise generated by quiet engine fans : III - fan C

    Noise generated by quiet engine fans : III - fan C by Montegani, Francis J.

    Washington : Springfield, Va. : for sale by the National Technical Information Service, U.S. National Aeronautics and Space Administration ; 1976
    Format: Government Document Book


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  3. 3
    Twelve month technical progress report to the National Aeronautics and Space Administration on NASA grant NSG-3048 alternatives for jet engine control November 1, 1983 - October 31, 1984

    Twelve month technical progress report to the National Aeronautics and Space Administration on NASA grant NSG-3048 alternatives for jet engine control November 1, 1983 - October 31... by Sain, Michael K.

    Notre Dame, Ind. : [Washington, D.C.] : University of Notre Dame, Dept. of Electrical Engineering ; National Aeronautics and Space Administration, 1984
    Format: Government Document Book


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  4. 4
    Some problems in the theory and assessment of turbo-jet engines

    Some problems in the theory and assessment of turbo-jet engines by Kholshchevnikov, Konstantin Vasilʹevich

    New York : Macmillan, 1964
    Format: Book


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  5. 5
    Measurement uncertaintyfor the uniform engine testing program conducted at the NASA Lewis Research Center

    Measurement uncertaintyfor the uniform engine testing program conducted at the NASA Lewis Research Center by Abdelwahab, Mahmood

    [Washington, DC : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1987
    Format: Government Document Book


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  6. 6
    Skyrocketing into the unknown

    Skyrocketing into the unknown by Coombs, Charles Ira, 1914-1994

    New York : Morrow, 1954
    Format: Book


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  7. 7
    Proceedings [held] April 16-19, 1963

    Proceedings [held] April 16-19, 1963

    Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command : [obtainable from the Defense Documentation Center for Scientific and Technical Information (DDC) Washington], 1963
    Format: Conference Proceeding Book


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  8. 8
    Automated procedure for developing hybrid computer simulations of turbofan engines

    Automated procedure for developing hybrid computer simulations of turbofan engines by Szuch, John R.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Format: Government Document Book


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  9. 9
    Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics

    Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics by Schweikhard, William G.

    Washington, D.C. : [Springfield, Va. : For sale by the National Technical Information Service], National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1983
    Format: Government Document Book


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  10. 10
    Oversight of FAA--reliability of "drilled" turbine fan blades on CF-6 engine used to power DC-10 and A-300B aircraft : hearings before the Special Subcommittee on Investigations of the Committee on Interstate and Foreign Commerce, House of Representatives, Ninety-third Congress, second session ... July 2 and 10, 1974.

    Oversight of FAA--reliability of "drilled" turbine fan blades on CF-6 engine used to power DC-10 and A-300B aircraft : hearings before the Special Subcommittee on Investigations of...

    Washington : U.S. Govt. Print. Off, 1974
    Format: Government Document Book


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  11. 11
    Perspectives on dilution jet mixing

    Perspectives on dilution jet mixing by Holdeman, J. D.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1986
    Format: Government Document Book


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  12. 12
    Effect of flame stabilizer design on performance and exhaust pollutants of a two-row swirl-can combustor operated to near-stoichiometric conditions

    Effect of flame stabilizer design on performance and exhaust pollutants of a two-row swirl-can combustor operated to near-stoichiometric conditions by Biaglow, James A.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  13. 13
    Aircraft engine controls : design, system analysis, and health monitoring

    Aircraft engine controls : design, system analysis, and health monitoring by Jaw, Link C.

    Reston, VA : American Institute of Aeronautics and Astronautics, 2009
    Format: Book


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  14. 14
    Computer program for estimating performance of air-breathing aircraft engines

    Computer program for estimating performance of air-breathing aircraft engines by Geiselhart, Karl A.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  15. 15
    A study of the effect of various fuels on the optimum length of a gas turbine combustor equipped with a vaporizer tube.

    A study of the effect of various fuels on the optimum length of a gas turbine combustor equipped with a vaporizer tube. by Barnes, Robert John

    1954
    Format: Thesis Book


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  16. 16
    An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0

    An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 by Re, Richard J.

    Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976
    Format: Government Document Book


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  17. 17
    The linear dynamics of a turbojet engine as developed from the linearized component equations.

    The linear dynamics of a turbojet engine as developed from the linearized component equations. by Schmidt, Ross Dean

    1955
    Format: Thesis Book


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  18. 18
    Advanced technology fuel mass flowmeter

    Advanced technology fuel mass flowmeter

    Fort Eustis, Va. : The Laboratory, 1978
    Format: Government Document Book


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  19. 19
    Marines and helicopters : 1946-1962

    Marines and helicopters : 1946-1962 by Rawlins, Eugene W.

    Washington, D.C. : History and Museums Division, Headquarters, U.S. Marine Corps, 1976
    Format: Government Document Book


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  20. 20
    Component-specific modeling second annual status report

    Component-specific modeling second annual status report by McKnight, R. L.

    Cleveland, Ohio : [Springfield, Va. : National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service, distributor, 1985
    Format: Government Document Book


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