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exhaust nozzles

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View Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20 By Lawrence E. Putnam

Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20

Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20

By Lawrence E. Putnam

View Ultra-high bypass ratio jet noise By Low, John, K. C.

Ultra-high bypass ratio jet noise

Ultra-high bypass ratio jet noise

By Low, John, K. C.

View Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control By Scott C. Asbury

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

By Scott C. Asbury

View Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle By Karen A. Deere

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

By Karen A. Deere

View Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft By Jack G. McArdle

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

By Jack G. McArdle

View Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft By Barbara S. Esker

Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft

Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft

By Barbara S. Esker

View Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft By Barbara S. Esker

Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

By Barbara S. Esker

View High speed nozzles task By A. Hamed

High speed nozzles task

High speed nozzles task

By A. Hamed

View Shelf life extension for the lot AAE nozzle severance LSCs By M. Cook

Shelf life extension for the lot AAE nozzle severance LSCs

Shelf life extension for the lot AAE nozzle severance LSCs

By M. Cook

View A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields By Nicholas J. Georgiadis

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields

By Nicholas J. Georgiadis

View Titanium aluminide applications in the high speed civil transport By Paul A. Bartolotta

Titanium aluminide applications in the high speed civil transport

Titanium aluminide applications in the high speed civil transport

By Paul A. Bartolotta

View Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector By Scott C. Asbury

Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

Internal performance of a fixed-shroud nonaxisymmetric nozzle equipped with an aft-hood exhaust deflector

By Scott C. Asbury

View Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept By David J. Wing

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

By David J. Wing

View Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application By Jagdish S. Sokhey

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application

By Jagdish S. Sokhey

View Analysis and design of optimized truncated scarfed nozzles subject to external flow effects By Rickey J. Shyne

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

By Rickey J. Shyne

View Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case By Joseph F. Baumeister

Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case

Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case

By Joseph F. Baumeister

View An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct By Bruce A. Reichert

An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct

An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct

By Bruce A. Reichert

View Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet By Michael K. Ponton

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet

By Michael K. Ponton

View Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility By Kin C. Wong

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

By Kin C. Wong

View Separate flow nozzle test status meeting By

Separate flow nozzle test status meeting

Separate flow nozzle test status meeting

By

View Separate flow nozzle test status meeting By United States. National Aeronautics and Space Administration. Scientific and Technical Information Program,NASA Glenn Research Center

Separate flow nozzle test status meeting

Separate flow nozzle test status meeting

By United States. National Aeronautics and Space Administration. Scientific and Technical Information Program,NASA Glenn Research Center

View Start up research effort in fluid mechanics By Samuel G. White

Start up research effort in fluid mechanics

Start up research effort in fluid mechanics

By Samuel G. White