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free flow

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View Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) By M. N. Kogan

Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)

Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)

By M. N. Kogan

View The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge By Peter W. Duck

The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge

The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge

By Peter W. Duck

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 Improved two-equation k - [omega] turbulence models for aerodynamic flows By Florian R. Menter

Improved two-equation k - [omega] turbulence models for aerodynamic flows

Improved two-equation k - [omega] turbulence models for aerodynamic flows

By Florian R. Menter

View Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)

Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction

Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction

By Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)

View Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data By R. C. Potter

Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data

Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data

By R. C. Potter

View Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6 By Floyd J. Wilcox

Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6

Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6

By Floyd J. Wilcox

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 The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity By Peter W. Duck

The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity

The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity

By Peter W. Duck

View Pressure distributions from subsonic tests of a NACA 0012 semispan wing model By Zachary T. Applin

Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

By Zachary T. Applin

View Summary report of the orbital X-34 wing static aeroelastic study By Ramadas K. Prabhu

Summary report of the orbital X-34 wing static aeroelastic study

Summary report of the orbital X-34 wing static aeroelastic study

By Ramadas K. Prabhu

View Detailed flow-field measurements over a 75⁰ swept delta wing By Scott O. Kjelgaard

Detailed flow-field measurements over a 75⁰ swept delta wing

Detailed flow-field measurements over a 75⁰ swept delta wing

By Scott O. Kjelgaard

View The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients By Jon A. Hoffmann

The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients

The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients

By Jon A. Hoffmann

View Effect of curvature on the impact damage characteritiscs and residual strength of composite plates By Damodar R. Ambur

Effect of curvature on the impact damage characteritiscs and residual strength of composite plates

Effect of curvature on the impact damage characteritiscs and residual strength of composite plates

By Damodar R. Ambur

View Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) By M. N. Kogan

Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)

Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)

By M. N. Kogan

View Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity By David L. Rigby

Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity

Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity

By David L. Rigby

View Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction By Francisco J. Cestero

Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction

Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction

By Francisco J. Cestero

View Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions By Ralph J. Volino

Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions

Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions

By Ralph J. Volino

View On the freestream matching condition for stagnation point turbulent flows By C. G. Speziale

On the freestream matching condition for stagnation point turbulent flows

On the freestream matching condition for stagnation point turbulent flows

By C. G. Speziale

View Towards enhancing and delaying disturbances in free shear flows By William O. Criminale

Towards enhancing and delaying disturbances in free shear flows

Towards enhancing and delaying disturbances in free shear flows

By William O. Criminale

View Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation By Klaus Rued

Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation

Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation

By Klaus Rued

View On the interaction between the shock wave attached to a wedge and freestream disturbances By Peter W. Duck

On the interaction between the shock wave attached to a wedge and freestream disturbances

On the interaction between the shock wave attached to a wedge and freestream disturbances

By Peter W. Duck

View Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor By Terence A. Ghee

Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor

Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor

By Terence A. Ghee

View Hypersonic flows about a 25 ̊sharp cone By James N. Moss

Hypersonic flows about a 25 ̊sharp cone

Hypersonic flows about a 25 ̊sharp cone

By James N. Moss