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axisymmetric flow

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View Self-similar compressible free vortices By Karl Von Ellenrieder

Self-similar compressible free vortices

Self-similar compressible free vortices

By Karl Von Ellenrieder

View Axisymmetric free shear flows with and without swirl By Alan Peter Morse

Axisymmetric free shear flows with and without swirl

Axisymmetric free shear flows with and without swirl

By Alan Peter Morse

View Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors By James F. Schmidt

Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors

Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors

By James F. Schmidt

View Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique By J. K. Ahuja

Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique

Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique

By J. K. Ahuja

View Enhanced mixing of an axisymmetric jet by aerodynamic excitation By Ganesh Raman

Enhanced mixing of an axisymmetric jet by aerodynamic excitation

Enhanced mixing of an axisymmetric jet by aerodynamic excitation

By Ganesh Raman

View Numerical investigations in the backflow region of a vacuum plume By G. S. Liaw

Numerical investigations in the backflow region of a vacuum plume

Numerical investigations in the backflow region of a vacuum plume

By G. S. Liaw

View Computer program BL2D for solving two-dimensional and axisymmetric boundary layers By Venkit Iyer

Computer program BL2D for solving two-dimensional and axisymmetric boundary layers

Computer program BL2D for solving two-dimensional and axisymmetric boundary layers

By Venkit Iyer

View Computing axisymmetric jet screech tones using unstructured grids By Philip C. E. Jorgenson

Computing axisymmetric jet screech tones using unstructured grids

Computing axisymmetric jet screech tones using unstructured grids

By Philip C. E. Jorgenson

View Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions By Y. Y. Chan

Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions

Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions

By Y. Y. Chan

View The design/analysis of flows through turbomachinery By D. P. Miller

The design/analysis of flows through turbomachinery

The design/analysis of flows through turbomachinery

By D. P. Miller

View An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies By Irina G. Brykina

An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies

An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies

By Irina G. Brykina

View Model of an aero-space plane based on an idealized cone-derived waverider forebody By Hyung-Koo Park

Model of an aero-space plane based on an idealized cone-derived waverider forebody

Model of an aero-space plane based on an idealized cone-derived waverider forebody

By Hyung-Koo Park

View Comparison of turbulence models for nozzle-afterbody flows with propulsive jets By William B. Compton

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets

By William B. Compton

View Supersonic jet noise reductions predicted with increased jet spreading rate By Milo D. Dahl

Supersonic jet noise reductions predicted with increased jet spreading rate

Supersonic jet noise reductions predicted with increased jet spreading rate

By Milo D. Dahl

View Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability By Mary L. Mason

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

By Mary L. Mason

View Comparison of 3D computation and experiment for non-axisymmetric nozzles By H. T. Lai

Comparison of 3D computation and experiment for non-axisymmetric nozzles

Comparison of 3D computation and experiment for non-axisymmetric nozzles

By H. T. Lai

View Experimental study of vortex breakdown in a cylindrical, swirling flow By

Experimental study of vortex breakdown in a cylindrical, swirling flow

Experimental study of vortex breakdown in a cylindrical, swirling flow

By

View Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation By Chin-Shun Lin

Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation

Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation

By Chin-Shun Lin

View Jets and flames in co-flowing streams By S. Ha

Jets and flames in co-flowing streams

Jets and flames in co-flowing streams

By S. Ha

View Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation By Clinton P. T. Groth

Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation

Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation

By Clinton P. T. Groth

View Spreading characteristics and thrust of jets from asymmetric nozzles By K. B. M. O. Zaman

Spreading characteristics and thrust of jets from asymmetric nozzles

Spreading characteristics and thrust of jets from asymmetric nozzles

By K. B. M. O. Zaman

View Calculations of diffuser flows with an anisotropic K-[epsilon] model By Chiang Chu

Calculations of diffuser flows with an anisotropic K-[epsilon] model

Calculations of diffuser flows with an anisotropic K-[epsilon] model

By Chiang Chu

View The filtered Abel transform and its application in combustion diagnostics By Zeng-Guang Yuan

The filtered Abel transform and its application in combustion diagnostics

The filtered Abel transform and its application in combustion diagnostics

By Zeng-Guang Yuan

View An outflow boundary condition for aeroacoustic computations By Ehteshamul Md Hayder

An outflow boundary condition for aeroacoustic computations

An outflow boundary condition for aeroacoustic computations

By Ehteshamul Md Hayder