<p>Left column (a-e) shows the dimensionless pressure distribution over the surface of the model and over a semisphere of radius 0.9<i>R</i> around the body point of reference. Middle column (f-j) shows the pressure iso-contours for two different takeoffs: N/m and 0.0430 N/m. Right column (k-o) compares iso-contours of the dimensionless vorticity magnitude for the same two takeoffs. Time instants are <i>t</i> = 24.73, 25.68, 26.63, 27.58 and 28.53 ms (<i>tf</i> = 5.2, 5.4 5.6, 5.8 and 6, where <i>f</i> is the wingbeat frequency).</p
lf~4.JABSTRACT ('1x'-'m~wr: ilaneuvering aircraft operate in rapidly changing, time-d...
A wide range of unsteady phenomena relevant to vortex flows over stationary and maneuvering delta wi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
<p>The vorticity iso-surfaces (blue: +<i>ω<sub>x</sub></i><sub> iso</sub>; red: −<i>ω<sub>x</sub></i...
<p>(A–D) OBW model at = 0.20, 0.33, 0.80 and 0.93 respectively. (E–F) FPW 1 model at = 0.33 and 0....
<p>Vorticity contours visualization at (a) (R<sub>e</sub>, g) = (75, 3) and (b) (R<sub>e</sub>, g) =...
<p>(A) Video sequences of the flight after take-off for fruitfly FF1. (B) Time histories of body pit...
<p>Instantaneous vorticity contours visualization corresponding to synchronous flow pattern for (a) ...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
<p>Five measurement phases from top to bottom rows are early systole, systolic peak, late systole, d...
Discernible trends in early vortex formation have been in inter vortex-plate distance, circulation, ...
<p>(a) T* = 0.05, (b)T* = 0.125, (c)T* = 0.2, (d)T* = 0.25, (e)T* = 0.325, (f)T* = 0.45, (g) T* = 0....
Vortex dynamics of more than 50 military wing configurations, such as diamond and delta wings with s...
The vortical flow over swept wings with several leading edge separations bears a number of challeng...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
lf~4.JABSTRACT ('1x'-'m~wr: ilaneuvering aircraft operate in rapidly changing, time-d...
A wide range of unsteady phenomena relevant to vortex flows over stationary and maneuvering delta wi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
<p>The vorticity iso-surfaces (blue: +<i>ω<sub>x</sub></i><sub> iso</sub>; red: −<i>ω<sub>x</sub></i...
<p>(A–D) OBW model at = 0.20, 0.33, 0.80 and 0.93 respectively. (E–F) FPW 1 model at = 0.33 and 0....
<p>Vorticity contours visualization at (a) (R<sub>e</sub>, g) = (75, 3) and (b) (R<sub>e</sub>, g) =...
<p>(A) Video sequences of the flight after take-off for fruitfly FF1. (B) Time histories of body pit...
<p>Instantaneous vorticity contours visualization corresponding to synchronous flow pattern for (a) ...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
<p>Five measurement phases from top to bottom rows are early systole, systolic peak, late systole, d...
Discernible trends in early vortex formation have been in inter vortex-plate distance, circulation, ...
<p>(a) T* = 0.05, (b)T* = 0.125, (c)T* = 0.2, (d)T* = 0.25, (e)T* = 0.325, (f)T* = 0.45, (g) T* = 0....
Vortex dynamics of more than 50 military wing configurations, such as diamond and delta wings with s...
The vortical flow over swept wings with several leading edge separations bears a number of challeng...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
lf~4.JABSTRACT ('1x'-'m~wr: ilaneuvering aircraft operate in rapidly changing, time-d...
A wide range of unsteady phenomena relevant to vortex flows over stationary and maneuvering delta wi...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...