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1

S, Litt Jonathan, Guo Ten-Huei, and Lewis Research Center, eds. Neural network-based sensor validation for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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2

S, Litt Jonathan, Guo Ten-Huei, and Lewis Research Center, eds. Neural network-based sensor validation for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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3

S, Litt Jonathan, Guo T. H, and Lewis Research Center, eds. Neural network-based sensor validation for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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4

S, Litt Jonathan, Guo Ten-Huei, and Lewis Research Center, eds. Neural network-based sensor validation for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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5

D'Angelo, Martin. Wide speed range turboshaft study. National Aeronautics and Space Administration, 1995.

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6

E, Paxson D., Schobeiri M. T, and United States. National Aeronautics and Space Administration., eds. Dynamic simulation of a wave rotor topped turboshaft engine. National Aeronautics and Space Administration, 1997.

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7

Chen, Ku, Litt Jonathan S, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. A simplified dynamic model of the T700 turboshaft engine. National Aeronautics and Space Administration, 1992.

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8

Karl, Owen A., United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Forced response testing of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, U.S. Army Research Laboratory, 1997.

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9

Karl, Owen A., and United States. National Aeronautics and Space Administration., eds. Forced response testing of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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10

Center, Ames Research, ed. A high fidelity real-time simulation of a small turboshaft engine. National Aeronautics and Space Administration, Ames Research Center, 1988.

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11

Ballin, Mark G. A high fidelity real-time simulation of a small turboshaft engine. Ames Research Center, 1988.

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12

Center, Ames Research, ed. A high fidelity real-time simulation of a small turboshaft engine. National Aeronautics and Space Administration, Ames Research Center, 1988.

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13

Center, Ames Research, ed. A high fidelity real-time simulation of a small turboshaft engine. National Aeronautics and Space Administration, Ames Research Center, 1988.

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14

L, Mattern Duane, Le Dzu K, and United States. National Aeronautics and Space Administration., eds. Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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15

L, Mattern Duane, Le Dzu K, and United States. National Aeronautics and Space Administration., eds. Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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16

Milner, Edward J. Simulating a small turboshaft engine in a real-time multiprocessor simulator (RTMPS) environment. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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17

A, Klann Gary, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Contingency power for a small turboshaft engine by using water injection into turbine cooling air. National Aeronautics and Space Administration, 1992.

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18

Green, Michael D. Model-based fault diagnosis for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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19

Green, Michael D. Model-based fault diagnosis for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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20

Green, Michael D. Model-based fault diagnosis for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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21

Ahmet, Duyar, Litt Jonathan S, and Lewis Research Center, eds. Model-based fault diagnosis for turboshaft engines. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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22

A, Delaney R., and United States. National Aeronautics and Space Administration., eds. Small engine technology. National Aeronautics and Space Administration, 1997.

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23

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. National Aeronautics and Space Administration, 1995.

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24

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. National Aeronautics and Space Administration, 1995.

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25

Litt, John. Sensor fault detection and diagnosis simulation of a helicopter engine in an intelligent control framework. National Aeronautics and Space Administration, 1994.

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26

Mehmet, Kurtkaya, Duyar Ahmet, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Sensor fault detection and diagnosis simulation of a helicopter engine in an intelligent control framework. National Aeronautics and Space Administration, 1994.

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27

Forced response testing of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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28

Forced response testing of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, U.S. Army Research Laboratory, 1997.

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29

A high fidelity real-time simulation of a small turboshaft engine. National Aeronautics and Space Administration, Ames Research Center, 1988.

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30

Contingency power for a small turboshaft engine by using water injection into turbine cooling air. National Aeronautics and Space Administration, 1992.

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31

Wave rotor-enhanced gas turbine engines. National Aeronautics and Space Administration, 1995.

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32

Wave engine topping cycle assessment. National Aeronautics and Space Administration, 1996.

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33

Contingency power for small turboshaft engines using water injection into turbine cooling air. National Aeronautics and Space Administration, 1987.

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34

Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor. National Aeronautics and Space Administration, 1996.

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