Add to ORKGAn experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF). The objective was to investigate the effects of Reynolds and Mach numbers on slender-wing leading-edge vortex flows with four values of wing leading-edge bluntness. Experimentally obtained pressure data are presented without analysis in tabulated and graphical formats across a Reynolds number range of 6 x 10(exp 6) to 36 x 10(exp 6) at a Mach number of 0.85 and across a Mach number range of 0.4 to 0.9 at a Reynolds number of 6 x 10(exp 6). Normal-force and pitching-moment coefficient plots for these Reynolds number and Mach number ranges are also presented
Detailed pressure measurements were made on a flat semispan swept wing with a rounded leading edge a...
A low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edge...
As part of a cooperative research program between NASA, McDonnell Douglas Corporation, and Wright Re...
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was...
A 65 o delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic chord...
Available experimental data on a 65xB0; swept back cropped delta wing with rounded leading edges hav...
The vortex properties over a delta wing depend mainly on angle of attack (α), Mach number (M), Reyno...
An investigation was conducted to study in detail the vortical flow over the leeward side of a 70 de...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
An experimental investigation of the effect of leading-edge radius, camber, Reynolds number, and bou...
The vortex dominated aerodynamic characteristics of a generic 65 degree cropped delta wing model wer...
A 65 deg delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic cho...
An assessment of the influence of airfoil geometry on delta wing leading edge vortex flow and vortex...
To understand Mach number effect on flow field over a delta wing with blunt leading edge in superson...
A review is presented of the initial experimental results and analysis that formed the basis the Vor...
Detailed pressure measurements were made on a flat semispan swept wing with a rounded leading edge a...
A low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edge...
As part of a cooperative research program between NASA, McDonnell Douglas Corporation, and Wright Re...
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was...
A 65 o delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic chord...
Available experimental data on a 65xB0; swept back cropped delta wing with rounded leading edges hav...
The vortex properties over a delta wing depend mainly on angle of attack (α), Mach number (M), Reyno...
An investigation was conducted to study in detail the vortical flow over the leeward side of a 70 de...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
An experimental investigation of the effect of leading-edge radius, camber, Reynolds number, and bou...
The vortex dominated aerodynamic characteristics of a generic 65 degree cropped delta wing model wer...
A 65 deg delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic cho...
An assessment of the influence of airfoil geometry on delta wing leading edge vortex flow and vortex...
To understand Mach number effect on flow field over a delta wing with blunt leading edge in superson...
A review is presented of the initial experimental results and analysis that formed the basis the Vor...
Detailed pressure measurements were made on a flat semispan swept wing with a rounded leading edge a...
A low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edge...
As part of a cooperative research program between NASA, McDonnell Douglas Corporation, and Wright Re...