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leading edges

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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 Numerical simulation of the SOFIA flowfield By Stephen P. Klotz

Numerical simulation of the SOFIA flowfield

Numerical simulation of the SOFIA flowfield

By Stephen P. Klotz

View High-lift systems on commercial subsonic airliners By Peter K. C. Rudolph

High-lift systems on commercial subsonic airliners

High-lift systems on commercial subsonic airliners

By Peter K. C. Rudolph

View Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements By W. Lance Richards

Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements

Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements

By W. Lance Richards

View Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters By John E. Lamar

Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters

Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters

By John E. Lamar

View A laser-based ice shape profilometer for use in icing wind tunnels By Edward A. Hovenac

A laser-based ice shape profilometer for use in icing wind tunnels

A laser-based ice shape profilometer for use in icing wind tunnels

By Edward A. Hovenac

View Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications By David E. Hahne

Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications

Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications

By David E. Hahne

View F-18 High Alpha Research Vehicle surface pressures By David F. Fisher

F-18 High Alpha Research Vehicle surface pressures

F-18 High Alpha Research Vehicle surface pressures

By David F. Fisher

View Finite element thermo-viscoplastic analysis of aerospace structures By Ajay K. Pandey

Finite element thermo-viscoplastic analysis of aerospace structures

Finite element thermo-viscoplastic analysis of aerospace structures

By Ajay K. Pandey

View Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip By V. K. Arya

Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip

Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip

By V. K. Arya

View SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions By R. Craig Robinson

SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions

SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions

By R. Craig Robinson

View Transonic Navier-Stokes calculations about a 65⁰ delta wing By W. Kelly Londenberg

Transonic Navier-Stokes calculations about a 65⁰ delta wing

Transonic Navier-Stokes calculations about a 65⁰ delta wing

By W. Kelly Londenberg

View Control of unsteady separated flow associated with the dynamic stall of airfoils By Michael C. Wilder

Control of unsteady separated flow associated with the dynamic stall of airfoils

Control of unsteady separated flow associated with the dynamic stall of airfoils

By Michael C. Wilder

View Compressible Navier-Stokes equations By S. I. Hariharan

Compressible Navier-Stokes equations

Compressible Navier-Stokes equations

By S. I. Hariharan

View 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet By M. Mizukami

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By M. Mizukami

View Lee-side flow over delta wings at supersonic speeds By David S. Miller

Lee-side flow over delta wings at supersonic speeds

Lee-side flow over delta wings at supersonic speeds

By David S. Miller

View Numerical studies of boundary-layer receptivity By Helen L. Reed

Numerical studies of boundary-layer receptivity

Numerical studies of boundary-layer receptivity

By Helen L. Reed

View 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet By Masashi Mizukami

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By Masashi Mizukami

View Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV By David F. Fisher

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV

By David F. Fisher

View The structure of separated flow regions occurring near the leading edge of airfoils, including transition By T. J. Mueller

The structure of separated flow regions occurring near the leading edge of airfoils, including transition

The structure of separated flow regions occurring near the leading edge of airfoils, including transition

By T. J. Mueller

View A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region By Edward C. Polhamus

A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region

A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region

By Edward C. Polhamus

View NASA/FAA Tailplane Icing Program By Thomas P. Ratvasky

NASA/FAA Tailplane Icing Program

NASA/FAA Tailplane Icing Program

By Thomas P. Ratvasky

View Flow over a leading edge with distributed roughness By Jerzy M. Floryan

Flow over a leading edge with distributed roughness

Flow over a leading edge with distributed roughness

By Jerzy M. Floryan

View Improving CPA-TSD steady pressure solutions through airfoil slope modification By

Improving CPA-TSD steady pressure solutions through airfoil slope modification

Improving CPA-TSD steady pressure solutions through airfoil slope modification

By