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Unsteady ejector performance : an experimental investigation using a pulsejet driver by Paxson, Daniel E.
Cleveland, Ohio : Hanover Md. :; Cleveland, Ohio : Hanover MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for AeroSpace Information, 2002Call Number: Loading…
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2
A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1990Call Number: Loading…
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3
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors by Paxson, Daniel E.
Cleveland, Ohio : Hanover, MD : Springfield, VA :; Cleveland, Ohio : Hanover, MD : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information ; National Technical Information Service [distributor], 1999Call Number: Loading…
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4
A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1990Call Number: Loading…
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5
Numerical assessment of four-part through-flow wave rotor cycles with passage height variation by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1997Call Number: Loading…
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6
A numerical model for dynamic wave rotor analysis by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Call Number: Loading…
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7
Wave augmented diffusers for centrifugal compressors by Paxson, Daniel E.
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998Call Number: Loading…
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8
Recent improvements to and validation of the one dimensional NASA wave rotor model by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Call Number: Loading…
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9
A general numerical model for wave rotor analysis by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1992Call Number: Loading…
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10
An improved numerical model for wave rotor design and analysis by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1992Call Number: Loading…
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11
A modified through-flow ware rotor cycle with combustor bypass ducts by Paxson, Daniel E.
[Cleveland, Ohio] : Springfield, Va. : National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service, distributor, 1998Call Number: Loading…
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12
A comparison between numerically modelled and experimentally measured loss mechanisms in wave rotors by Paxson, Daniel E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1993Call Number: Loading…
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13
Jet engine performance enhancement through use of a wave-rotor topping cycle by Wilson, Jack
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993Other Authors: “…Paxson, Daniel E.…”
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14
Static flow characteristics of a mass flow injecting valve by Mattern, Duane L.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Other Authors: “…Paxson, Daniel E.…”
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15
Optimization of wave rotors for use as gas turbine engine topping cycles by Wilson, Jack
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Other Authors: “…Paxson, Daniel E.…”
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16
A simplified model for the investigation of acoustically driven combustion instabilities by Quinn, D. Dane
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998Other Authors: “…Paxson, Daniel E.…”
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17
Dynamic simulation of a wave rotor topped turboshaft engine by Greendyke, Robert B.
[Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1997Other Authors: “…Paxson, Daniel E.…”
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18
Wave rotor-enhanced gas turbine engines by Welch, Gerard E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Other Authors:Call Number: Loading…
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Related Subjects
Computational fluid dynamics
Rotors
Gas turbine engines
Unsteady flow
Combustion chambers
Gas-turbines
Mathematical models
Rotor aerodynamics
Space shuttles
Turboshafts
Acoustic instability
Airplanes
Bypass ratio
Centrifugal compressors
Centrifugal force
Combustion
Combustion stability
Compression waves
Compressors
Computer simulation
Computerized simulation
Design analysis
Ducted flow
Dynamic characteristics
Ejectors
Elastic waves
Engine design
Equations of motion
Exhaust gases
Fatigue