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Pressure ratio
Computational fluid dynamics 9
Nozzle design 6
Aerodynamic noise 4
Convergent-divergent nozzles 4
Exhaust nozzles 4
Flow distribution 4
Turbofan engines 4
Centrifugal compressors 3
Noise reduction 3
Nozzle flow 3
Performance tests 3
Plumes 3
Supersonic aircraft 3
Wind tunnel tests 3
Acoustic properties 2
Aeroacoustics 2
Aerodynamics 2
Compressors 2
Design analysis 2
Detonation 2
Ducted fans 2
Ejectors 2
Elastic waves 2
Engine design 2
Engine inlets 2
Fan blades 2
Jet aircraft noise 2
Laminar flow 2
Low speed wind tunnels 2

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

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.

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

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

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

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

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

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

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.

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

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

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

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

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

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

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)

Computational study of the CC3 impeller and vaneless diffuser experiment / by Kulkarni, Sameer, Beach, Timothy A., Skoch, Gary J.

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-

High speed nozzles task final report / by Hamed, A. (Awatef)

Coordinates for a high performance 4:1 pressure ratio centrifugal compressor by McKain, Ted F.

Search Results

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

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.

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

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

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

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

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

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

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.

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

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

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

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

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

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

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)

Computational study of the CC3 impeller and vaneless diffuser experiment / by Kulkarni, Sameer, Beach, Timothy A., Skoch, Gary J.

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-

High speed nozzles task final report / by Hamed, A. (Awatef)

Coordinates for a high performance 4:1 pressure ratio centrifugal compressor by McKain, Ted F.

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