Tomeki

Explore Books on
inlet flow

1-24 of 48 Books

View Numerical simulation of the flow about the F-18 HARV at high angle of attack By Scott M. Murman

Numerical simulation of the flow about the F-18 HARV at high angle of attack

Numerical simulation of the flow about the F-18 HARV at high angle of attack

By Scott M. Murman

View A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application By Kamlesh Kapoor

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

By Kamlesh Kapoor

View IPAC--Inlet Performance Analysis Code By Paul J. Barnhart

IPAC--Inlet Performance Analysis Code

IPAC--Inlet Performance Analysis Code

By Paul J. Barnhart

View Reduction of Blade-Vortex Interaction (BVI) noise through X-force control By Fredric H. Schmitz

Reduction of Blade-Vortex Interaction (BVI) noise through X-force control

Reduction of Blade-Vortex Interaction (BVI) noise through X-force control

By Fredric H. Schmitz

View Research on a two-dimensional inlet for a supersonic V/STOL propulsion system By J. L. Mark

Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

By J. L. Mark

View Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study By C. Frederic Smith

Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study

Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study

By C. Frederic Smith

View Comparison of the aeroacoustics of two small-scale supersonic inlets By Wing Ng

Comparison of the aeroacoustics of two small-scale supersonic inlets

Comparison of the aeroacoustics of two small-scale supersonic inlets

By Wing Ng

View Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code By Kamlesh Kapoor

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

By Kamlesh Kapoor

View Control of flow separation and mixing by aerodynamic excitation By Edward J. Rice

Control of flow separation and mixing by aerodynamic excitation

Control of flow separation and mixing by aerodynamic excitation

By Edward J. Rice

View Mach 10 experimental database of a three-dimensional scramjet inlet flow field By Scott D. Holland

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

By Scott D. Holland

View Numerical simulation of supersonic and hypersonic inlet flow fields By D. Scott McRae

Numerical simulation of supersonic and hypersonic inlet flow fields

Numerical simulation of supersonic and hypersonic inlet flow fields

By D. Scott McRae

View Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels By James C. Ross

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels

By James C. Ross

View An experimental device for generating high frequency perturbations in supersonic wind tunnels By Kevin J. Melcher

An experimental device for generating high frequency perturbations in supersonic wind tunnels

An experimental device for generating high frequency perturbations in supersonic wind tunnels

By Kevin J. Melcher

View LDV measurements in an annular combustor model By Dean A. Barron

LDV measurements in an annular combustor model

LDV measurements in an annular combustor model

By Dean A. Barron

View Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 By Scott Douglas Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

By Scott Douglas Holland

View Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane By William G. Steenken

Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane

Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane

By William G. Steenken

View Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics By J. R. DeBonis

Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics

Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics

By J. R. DeBonis

View Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion By M. K. Ghosh

Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion

Starvation effects on the hydrodynamic lubrication of rigid nonconformal contacts in combined rolling and normal motion

By M. K. Ghosh

View Numerical calculation of scramjet inlet flow By Tomiko Ishiguro

Numerical calculation of scramjet inlet flow

Numerical calculation of scramjet inlet flow

By Tomiko Ishiguro

View Inlet analysis using computational fluid dynamics By L. G. Hunter

Inlet analysis using computational fluid dynamics

Inlet analysis using computational fluid dynamics

By L. G. Hunter

View A numerical simulation of two-dimensional inlet flow fields By S. Birignen

A numerical simulation of two-dimensional inlet flow fields

A numerical simulation of two-dimensional inlet flow fields

By S. Birignen

View Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack By Crawford F. Smith

Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

By Crawford F. Smith

View Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets By Bernhard H. Anderson

Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets

Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets

By Bernhard H. Anderson

View The effects of vortex ingestion on the flow in a diffusing S-duct By B. J. Wendt

The effects of vortex ingestion on the flow in a diffusing S-duct

The effects of vortex ingestion on the flow in a diffusing S-duct

By B. J. Wendt