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1
Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level /
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2
Turbulent chemical interaction models in NCC comparison /
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3
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4
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5
Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines
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6
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7
Two phase flow modeling summary of flow regimes and pressure drop correlations in reduced and partial gravity /
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8
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9
Boundary layer flow control by an array of ramp-shaped vortex generators
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10
Comparison of tomo-PIV versus dual plane PIV on a synthetic jet flow /
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11
Summary of pressure gain combustion research at NASA /
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12
Understanding and mitigating tip leakage and endwall losses in high pressure ratio cores /
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13
Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests)
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14
Inlet flow control and prediction technologies for embedded propulsion systems summary report for fiscal year 2009 /
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15
A simplified model for detonation based pressure-gain combustors
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16
Measurements of turbulent flow field in separate flow nozzles with enhanced mixing devices, test report /
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17
Design and analysis tool for external-compression supersonic inlets
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18
Heat entrapment effects within liquid acquisition devices
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19
Harmonic balance computations of fan aeroelastic stability
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20
Measurements of a turbulent horseshoe vortex formed around a cylinder
Published: United Technologies Research Center ; National Aeronautics and Space Administration, Lewis Research Center, 1986Get full text
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