Two-Dimensional Simulations of Wake Vortex Detection Using Radio Acoustic Sounding Systems

AIAA Journal ◽  
2002 ◽  
Vol 40 (11) ◽  
pp. 2247-2256 ◽  
Author(s):  
Said Boluriaan ◽  
Philip J. Morris
Keyword(s):  
Wake Vortex ◽  
Two Dimensional ◽  
Acoustic Sounding ◽  
Vortex Detection

Numerical simulation of wake vortex detection using a radio acoustic sounding system

AIAA Journal ◽  
2001 ◽  
Vol 39 ◽  
pp. 1097-1105
Author(s):  
Said Boluriaan ◽  
Philip J. Morris
Keyword(s):  
Numerical Simulation ◽  
Wake Vortex ◽  
Acoustic Sounding ◽  
Vortex Detection

Numerical Simulation of Wake Vortex Detection Using a Radio Acoustic Sounding System

AIAA Journal ◽  
2001 ◽  
Vol 39 (6) ◽  
pp. 1097-1105 ◽  
Author(s):  
Said Boluriaan ◽  
Philip J. Morris
Keyword(s):  
Numerical Simulation ◽  
Wake Vortex ◽  
Acoustic Sounding ◽  
Vortex Detection

Wake Vortex Detection and Tracking for Aircraft Formation Flight

2021 ◽  
pp. 1-19
Author(s):  
Ignace Ransquin ◽  
Denis-Gabriel Caprace ◽  
Matthieu Duponcheel ◽  
Philippe Chatelain
Keyword(s):  
Formation Flight ◽  
Wake Vortex ◽  
Detection And Tracking ◽  
Vortex Detection

scholarly journals Ultrasonic Method for Aircraft Wake Vortex Detection

2007 ◽  
Vol 44 (3) ◽  
pp. 726-732 ◽  
Author(s):  
Rebecca J. Rodenhiser ◽  
William W. Durgin ◽  
Hamid Johari
Keyword(s):  
Ultrasonic Method ◽  
Wake Vortex ◽  
Aircraft Wake ◽  
Vortex Detection

A Note on the Estimation of Average Pressures from Instantaneous Velocities in Unsteady Flow

1967 ◽  
Vol 71 (678) ◽  
pp. 440-440
Author(s):  
C. J. Wood
Keyword(s):  
Unsteady Flow ◽  
Boundary Layers ◽  
Data Reduction ◽  
Bluff Body ◽  
Wake Vortex ◽  
Two Dimensional ◽  
Experimental Check ◽  
Velocity Measurements ◽  
Periodic Disturbance ◽  
Oncoming Stream

In a recent paper, the author described some experiments in which the average base pressure on a two-dimensional bluff body was estimated from a random sample of instantaneous velocity measurements taken in the irrotational flow outside the separating boundary layers at the trailing edge. Although the oncoming stream was steady, the flow near the model was subject to a periodic disturbance emanating from the wake vortex street. An experimental check showed that the pressure estimates obtained by using the steady Bernouilli equation were reasonably accurate. This note points out that the method of data reduction used in ref. 1 is not an approximation; it is exact.

Pulsed 1.5-$\mu$m LIDAR for Axial Aircraft Wake Vortex Detection Based on High-Brightness Large-Core Fiber Amplifier

2009 ◽  
Vol 15 (2) ◽  
pp. 441-450 ◽  
Author(s):  
A. Dolfi-Bouteyre ◽  
G. Canat ◽  
M. Valla ◽  
B. Augere ◽  
C. Besson ◽  
...  
Keyword(s):  
Fiber Amplifier ◽  
Wake Vortex ◽  
Large Core ◽  
High Brightness ◽  
Aircraft Wake ◽  
Vortex Detection ◽  
Core Fiber
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