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ejectors

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View A control-volume method for analysis of unsteady thrust augmenting ejector flows By Colin K. Drummond

A control-volume method for analysis of unsteady thrust augmenting ejector flows

A control-volume method for analysis of unsteady thrust augmenting ejector flows

By Colin K. Drummond

View A model for prediction of STOVL ejector dynamics By Colin K. Drummond

A model for prediction of STOVL ejector dynamics

A model for prediction of STOVL ejector dynamics

By Colin K. Drummond

View A modeling technique for STOVL ejector and volume dynamics By Colin K. Drummond

A modeling technique for STOVL ejector and volume dynamics

A modeling technique for STOVL ejector and volume dynamics

By Colin K. Drummond

View Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight By Scott R. Thomas

Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight

Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight

By Scott R. Thomas

View Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector By Wendy S. Barankiewicz

Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector

Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector

By Wendy S. Barankiewicz

View Supersonic ejectors By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Supersonic ejectors

Supersonic ejectors

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

View Lobed mixer optimization for advanced ejector geometries By Ian A. Waitz

Lobed mixer optimization for advanced ejector geometries

Lobed mixer optimization for advanced ejector geometries

By Ian A. Waitz

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 Transient flow thrust prediction for an ejector propulsion concept By Colin K. Drummond

Transient flow thrust prediction for an ejector propulsion concept

Transient flow thrust prediction for an ejector propulsion concept

By Colin K. Drummond

View Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system By Nicholas J. Georgiadis

Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system

Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system

By Nicholas J. Georgiadis

View Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows By Lawrence Justin DeChant

Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows

Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows

By Lawrence Justin DeChant

View Design and calibration of an air ejector to operate against various back pressures By Ronald G. A. Chisholm

Design and calibration of an air ejector to operate against various back pressures

Design and calibration of an air ejector to operate against various back pressures

By Ronald G. A. Chisholm

View Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction By John F. Brausch

Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction

Simulated flight acoustic investigtion of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction

By John F. Brausch

View Thrust augmentation measurements using a pulse detonation engine ejector By Robert J. Santoro

Thrust augmentation measurements using a pulse detonation engine ejector

Thrust augmentation measurements using a pulse detonation engine ejector

By Robert J. Santoro

View Unsteady ejector performance By Daniel E. Paxson

Unsteady ejector performance

Unsteady ejector performance

By Daniel E. Paxson

View Effect of delta tabs on free jets from complex nozzles By K. B. M. Q. Zaman

Effect of delta tabs on free jets from complex nozzles

Effect of delta tabs on free jets from complex nozzles

By K. B. M. Q. Zaman

View Preliminary dynamic tests of a flight-type ejector By Colin K. Drummond

Preliminary dynamic tests of a flight-type ejector

Preliminary dynamic tests of a flight-type ejector

By Colin K. Drummond

View Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle By William Herkes

Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle

Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle

By William Herkes

View Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983 By D. B. Garland

Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983

Phase 4 static tests of the J-97 powered, external augmentor V/STOL model at the NASA, Ames Research Center, November 1983

By D. B. Garland