Add to ORKGA review is presented of the initial experimental results and analysis that formed the basis the Vortex Flow Experiment 2 (VFE-2). The focus of this work was to distinguish the basic effects of Reynolds number, Mach number, angle of attack, and leading edge bluntness on separation-induced leading-edge vortex flows that are common to slender wings. Primary analysis is focused on detailed static surface pressure distributions, and the results demonstrate significant effects regarding the onset and progression of leading-edge vortex separation. 18.2 NOMENCLATURE d = sting diameter Cp * = sonic pressure coefficient LTPT = Low Turbulence Pressure Tunnel mac = mean aerodynamic chord, (2/3) cr NTF = National Transonic Facility rle = streamwise le...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
The present work is investigating the vortex dominated flow physics as well as the aerodynamic behav...
A review is presented of the initial experimental results and analysis that formed the basis the Vor...
This paper discusses further the effects of Reynolds number, angle of attack and leading edge bluntn...
The flow behaviour over the upper surface of a blunt-edged delta wing is mainly governed by a compli...
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...
A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender ...
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was...
A 65 deg delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic cho...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Leading edge vortex (LEV) formation, which is initiated by separation at the leading edge, depends o...
The main objective of this project is to investigate the flow characteristics of the VFE- 2 blunt ed...
This thesis covers the field of vortex-flow dominated external aerodynamics. As part of the contribu...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
The present work is investigating the vortex dominated flow physics as well as the aerodynamic behav...
A review is presented of the initial experimental results and analysis that formed the basis the Vor...
This paper discusses further the effects of Reynolds number, angle of attack and leading edge bluntn...
The flow behaviour over the upper surface of a blunt-edged delta wing is mainly governed by a compli...
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...
A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender ...
An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was...
A 65 deg delta wing has been tested in the National Transonic Facility (NTF) at mean aerodynamic cho...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Leading edge vortex (LEV) formation, which is initiated by separation at the leading edge, depends o...
The main objective of this project is to investigate the flow characteristics of the VFE- 2 blunt ed...
This thesis covers the field of vortex-flow dominated external aerodynamics. As part of the contribu...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
The present work is investigating the vortex dominated flow physics as well as the aerodynamic behav...