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Book
Cracking in pressurizer safety and relief nozzles and in surge line nozzle
Author:
Year: 2004 Publisher: Washington, D.C. : U.S. Nuclear Regulatory Commission, Office of Nuclear Reactor Regulation,

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Abstract

Keywords

Nozzles --- Cracking.


Book
Leakage found on bottom-mounted instrumentation nozzles
Author:
Year: 2003 Publisher: Washington, D.C. : U.S. Nuclear Regulatory Commission, Office of Nuclear Reactor Regulation,

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Keywords

Nozzles. --- Boron.


Book
Two dimensional inviscid jet flow from two nozzles at an angle to a plane surface
Authors: --- --- ---
Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Book
Assessment and development of methods of acoustic performance prediction for jet noise suppressors
Authors: --- ---
Year: 1969 Publisher: Toronto: Institute for aerospace studies,

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Keywords

Jet planes --- Nozzles


Book
Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
Authors: --- --- ---
Year: 1988 Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division,

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Keywords

Jet nozzles --- Testing.


Book
Some characteristics of fuel sprays at low-injection pressures
Authors: --- ---
Year: 1931 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Keywords

Fuel. --- Aerosols. --- Nozzles. --- Injectors.


Book
The effect of injection-valve opening pressure on spray-tip penetration
Authors: --- ---
Year: 1931 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Abstract

Keywords

Nozzles. --- Injectors. --- Aerosols.


Book
Effect of orifice length-diameter ratio on spray characteristics
Authors: ---
Year: 1930 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Abstract

Keywords

Aerosols. --- Nozzles. --- Holes.


Book
Some characteristics of sprays obtained from pintle-type injection nozzles
Authors: --- ---
Year: 1933 Publisher: Washington [D.C.] : National Advisory Committee for Aeronautics,

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Abstract

Keywords

Atomization. --- Nozzles. --- Injectors.


Book
The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
Authors: --- ---
Year: 1953 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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