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  1. 1
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / by Berrier, Bobby L., Re, Richard J.

    Published 1980
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  2. 2
    Numerical assessment of four-port through-flow wave rotor cycles with passage height variation /

    Numerical assessment of four-port through-flow wave rotor cycles with passage height variation / by Paxson, Daniel E., Lindau, Jules W.

    Published 1997
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  3. 3
    Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

    Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters by Bare, E. Ann

    Published 1989
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  4. 4
    Calibration of sonic valves for the laminar flow control, leading-edge flight test /

    Calibration of sonic valves for the laminar flow control, leading-edge flight test /

    Published 1985
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  5. 5
    A performance map for ideal air breathing pulse detonation engines

    A performance map for ideal air breathing pulse detonation engines by Paxon, Daniel E.

    Published 2001
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  6. 6
    Multi-objective optimization of a turbofan for an advanced, single-aisle transport

    Multi-objective optimization of a turbofan for an advanced, single-aisle transport by Berton, Jeffrey J.

    Published 2012
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  7. 7
    Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models

    Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models by Jeracki, Robert J.

    Published 2006
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  8. 8
    Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility

    Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility by Werner, Roger A.

    Published 2010
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  9. 9
    CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /

    CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report / by Vinci, Samuel J.

    Published 2012
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  10. 10
    Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller

    Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller by Schumann, Lawrence F.

    Published 1986
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  11. 11
    Perceived noise analysis for offset jets applied to commercial supersonic aircraft /

    Perceived noise analysis for offset jets applied to commercial supersonic aircraft / by Huff, Dennis L.

    Published 2019
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  12. 12
    Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade /

    Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / by Ameri, Ali A.

    Published 2012
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  13. 13
    Exhaust nozzle plume effects on sonic boom test results for vectored nozzles

    Exhaust nozzle plume effects on sonic boom test results for vectored nozzles by Castner, Raymond S.

    Published 2012
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  14. 14
    Exhaust nozzle plume effects on sonic boom test results for isolated nozzles

    Exhaust nozzle plume effects on sonic boom test results for isolated nozzles by Castner, Raymond S.

    Published 2011
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  15. 15
    Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines

    Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines by Paxson, Daniel E.

    Published 2012
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  16. 16
    Preliminary aerodynamic investigation of fan rotor blade morphing /

    Preliminary aerodynamic investigation of fan rotor blade morphing / by Tweedt, Daniel L. (Daniel Lawrence)

    Published 2012
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  17. 17
    Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D /

    Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D / by Bartels, Robert E.

    Published 2012
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  18. 18
    The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows final grant report, NASA Langley grant NAG-1-1240, covering the period March 1991 to March 1993 /

    The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows final grant report, NASA Langley grant NAG-1-1240, covering the period March 1991 to... by Dosanjh, Darshan S., 1921-

    Published 1995
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  19. 19
    The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /

    The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / by Bozak, Richard F., Hughes, Christopher E., Buckley, James (Mechanical engineer)

    Published 2013
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  20. 20
    Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 final report /

    Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 final report / by Hwang, Kyu C.

    Published 1995
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