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Richard A. Rudey
Observed names:
R. A. Rudey,
R. RUDEY,
Rudey, R. A.
Institution:
Glenn Research Center
Observed institution:
Glenn Research Center
OpenAlex ID:
A5073514031
Characteristics and combustion of future hydrocarbon fuels
1978
·
R. A. Rudey
, J. S. Grobman
·
NASA STI Repository (National Aeronautics and Space Administration)
·
9
PDF
Technology for Reducing Aircraft Engine Pollution
1975
·
Richard A. Rudey
, Erwin E. Kempke
·
SAE technical papers on CD-ROM/SAE technical paper series
·
7
Measurement of high-altitude air quality using aircraft
1973
·
R. RUDEY
, P. PERKINS
·
International Conference on the Environmental Impact of Aerospace Operations in the High Atmosphere
·
4
A Review of NASA Combustor and Turbine Heat Transfer Research
1984
·
Richard A. Rudey
, Robert W. Graham
·
3
Impact of future fuel properties on aircraft engines and fuel systems
1978
·
R. A. Rudey
, J. S. Grobman
·
NASA Technical Reports Server (NASA)
·
3
Status review of NASA programs for reducing aircraft gas turbine engine emissions
1976
·
R. A. Rudey
·
NASA STI Repository (National Aeronautics and Space Administration)
·
3
PDF
Status of Technological Advancements for Reducing Aircraft Gas Turbine Engine Pollutant Emissions
1975
·
R. A. Rudey
·
NASA STI Repository (National Aeronautics and Space Administration)
·
2
PDF
Upper atmosphere pollution measurements (GASP)
1975
·
R. A. Rudey
, J. D. Holdeman
·
NASA STI Repository (National Aeronautics and Space Administration)
·
2
PDF
Effect of broadened-specification fuels on aircraft engines and fuel systems
1979
·
R. RUDEY
·
International Symposium on Air Breathing Engines (ISABE)
·
1
PDF
The Impact of Emission Standards on the Design of Aircraft Gas Turbine Engine Combustors
1976
·
Richard A. Rudey
·
SAE technical papers on CD-ROM/SAE technical paper series
·
1
Advanced combustion techniques for controlling NO sub x emissions of high altitude cruise aircraft
1976
·
R. A. Rudey
, Gregory M. Reck
·
NASA Technical Reports Server (NASA)
·
1
Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA Run 1
1964
·
T. J. Biesiadny
, R. J. Coltrin
, et al.
·
NASA Technical Reports Server (NASA)
·
1
PDF
Nuclear rocket simulator tests flow initiation with turbine accelerated tank pressure 50 PSIA, Run 11
1964
·
R. E. Coltrin
, T. C. Litzler
, et al.
·
NASA Technical Reports Server (NASA)
·
1
Advanced combustion techniques for controlling NO/x/ emissions of high altitude cruise aircraft
1976
·
R. A. Rudey
, Gregory M. Reck
·
NASA Technical Reports Server (NASA)
Technology for controlling emissions of oxides of nitrogen from supersonic cruise aircraft
1976
·
Gregory M. Reck
, R. A. Rudey
·
NASA Technical Reports Server (NASA)
PDF
Status of NASA aircraft engine emission reduction and upper atmosphere measurement programs
1976
·
R. A. Rudey
, E. A. Lezberg
·
NASA Technical Reports Server (NASA)
The impact of emissions standards on the design of aircraft gas turbine engine combustors
1976
·
R. A. Rudey
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
The long term energy problem and aeronautics
1975
·
R. A. Rudey
·
NASA Technical Reports Server (NASA)
Aircraft engine pollution reduction.
1972
·
R. A. Rudey
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
Effects of engine inlet disturbances on engine stall performance
1971
·
Frank W. Burcham
, J. E. Calogeras
, et al.
·
NASA Technical Reports Server (NASA)
Propellant flow system components
1966
·
Melvin J. Hartmann
, D. J. Connolley
, et al.
·
NASA Technical Reports Server (NASA)
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Works count:
25
Citation count:
38
H-index:
3
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