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jet nozzles

1-24 of 86 Books

View Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles By P. D. Thomas

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

By P. D. Thomas

View Boundary-layer separation on isolated boattail nozzles By William Kelly Abeyounis

Boundary-layer separation on isolated boattail nozzles

Boundary-layer separation on isolated boattail nozzles

By William Kelly Abeyounis

View Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle By Scott C. Asbury

Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

By Scott C. Asbury

View Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application By B. A. Janardan

Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application

Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application

By B. A. Janardan

View Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes By Robert J. Foley

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

By Robert J. Foley

View User's guide for the NOZL3D and NOZLIC computer programs By P. D. Thomas

User's guide for the NOZL3D and NOZLIC computer programs

User's guide for the NOZL3D and NOZLIC computer programs

By P. D. Thomas

View Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics By Laurence D. Leavitt

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

By Laurence D. Leavitt

View Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds By E. Ann Bare

Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds

Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds

By E. Ann Bare

View Evaluation of flip-flop jet nozzles for use as practical excitation devices By Raman Ganesh

Evaluation of flip-flop jet nozzles for use as practical excitation devices

Evaluation of flip-flop jet nozzles for use as practical excitation devices

By Raman Ganesh

View Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles By Verlon L. Head

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles

By Verlon L. Head

View Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression By James R. DeBonis

Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression

Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression

By James R. DeBonis

View Viscous computations of cold air/airflow around scramjet nozzle afterbody By Oktay Baysal

Viscous computations of cold air/airflow around scramjet nozzle afterbody

Viscous computations of cold air/airflow around scramjet nozzle afterbody

By Oktay Baysal

View Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement By Carpenter, Thomas.

Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement

Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement

By Carpenter, Thomas.

View Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement By Thomas W. Carpenter

Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement

Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement

By Thomas W. Carpenter

View Experimental results of a deflected thrust V/STOL nozzle research program By Paul L. Burstadt

Experimental results of a deflected thrust V/STOL nozzle research program

Experimental results of a deflected thrust V/STOL nozzle research program

By Paul L. Burstadt

View Jet engine hot parts IR analysis procedure (J-EIRP) By Joseph F. Baumeister

Jet engine hot parts IR analysis procedure (J-EIRP)

Jet engine hot parts IR analysis procedure (J-EIRP)

By Joseph F. Baumeister

View Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 By Francis J Capone

Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20

Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20

By Francis J Capone

View Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps By Laurence D. Leavitt

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

By Laurence D. Leavitt

View Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 By George T. Carson

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20

By George T. Carson

View Viscous three-dimensional analyses for nozzles for hypersonic propulsion By G. J. Harloff

Viscous three-dimensional analyses for nozzles for hypersonic propulsion

Viscous three-dimensional analyses for nozzles for hypersonic propulsion

By G. J. Harloff

View Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions By George T. Carson

Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions

Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions

By George T. Carson

View Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers By Odis C. Pendergraft

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers

By Odis C. Pendergraft

View Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles By Verlon L Head

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles

By Verlon L Head

View Measurements of the noise of air jets from slot nozzles with and without shields By F. -R Grosche

Measurements of the noise of air jets from slot nozzles with and without shields

Measurements of the noise of air jets from slot nozzles with and without shields

By F. -R Grosche