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11 works

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BOOKS

Books

10 total

Thermodynamic effects of cavitation of an 80.6 ̊helical inducer operated in hydrogen / Royce D. Moore and Phillip R. Meng.

Royce D. Moore

1970

Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage / Royce D. Moore and Walter M. Osborn.

Royce D. Moore

1979

Venturi Scaling Studies on Thermodynamic Effects of Developed Cavitation of Freon-114 / Royce D. Moore, Robert S. Ruggeri.

Royce D. Moore

1968

Performance of a low-pressure fan stage with reverse flow / Royce D. Moore, George W. Lewis, Jr., and Edward R. Tysl.

Royce D. Moore

1976

Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage / Walter M. Osborn, Royce D. Moore, and Ronald J. Steinke, Lewis Research Center.

Walter Martin Osborn

1978

Effect of blade leading edge thickness on cavitation performance of 80.6 ̊helical inducer in hydrogen / Royce D. Moore and Phillip R. Meng.

Royce D. Moore

1970

Comparison of noncavitation and cavitation performance for 78,̊ 80.6,̊ and 84 ̊helical inducers operated in hydrogen / Royce D. Moore and Phillip R. Meng.

Royce D. Moore

1971

DOCUMENTS · SCRIBD

Documents

4 total

Royce v. Moore: Habeas Corpus Appeal

Scribd Government Docs

Plato

Mirela

Moore v. Director: Black Lung Benefits Reversed

Scribd Government Docs

Reception of Alexander the Great

Sasha Pozelli

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3 of 10

Aerodynamic Performance of Axial-flow Fan Stage Operated at Nine Inlet Guide Vane Angles / Royce D. Moore and Lonnie Reid.

Royce D. Moore

1979

Prediction of Thermodynamic Effects of Developed Cavitation Based on Liquid-hydrogen and Freon-114 Data in Scaled Venturis / Royce D. Moore, Robert S. Ruggeri.

Royce D. Moore

1968

Performance of 1.15-pressure-ratio Fan Stage at Several Rotor Blade Setting Angles with Reverse Flow / George Kovich and Royce D. Moore.

George. Kovich

1976

Genres

Books

Thermodynamic effects of cavitation of an 80.6 ̊helical inducer operated in hydrogen / Royce D. Moore and Phillip R. Meng.

Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage / Royce D. Moore and Walter M. Osborn.

Venturi Scaling Studies on Thermodynamic Effects of Developed Cavitation of Freon-114 / Royce D. Moore, Robert S. Ruggeri.

Performance of a low-pressure fan stage with reverse flow / Royce D. Moore, George W. Lewis, Jr., and Edward R. Tysl.

Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage / Walter M. Osborn, Royce D. Moore, and Ronald J. Steinke, Lewis Research Center.

Effect of blade leading edge thickness on cavitation performance of 80.6 ̊helical inducer in hydrogen / Royce D. Moore and Phillip R. Meng.

Comparison of noncavitation and cavitation performance for 78,̊ 80.6,̊ and 84 ̊helical inducers operated in hydrogen / Royce D. Moore and Phillip R. Meng.