Calculated for the cross-sections taken at the base of the tail flukes of the L. albirostris, T. truncatus, G. melas and SD8020 airfoil at the averaged Re 4.77E+05 for the fluke’s cross-sections (Table 10).</p
Equations and design charts are given for predicting the downwash angles and the wake characteristic...
Averaged lift and drag coeffficients of a DU00-W-212 profile in laminar flow (background turbulence ...
<p>The lift to drag (L/D) performance of both the bio-realistic (bio) and flat wings plotted against...
Calculated for the cross-sections taken at the base of the tail flukes of the P. phocoena, D. delphi...
Comparison of the chord-normalized profile coordinates of cross-sections taken at the base and top o...
Comparison of the hydrodynamic characteristics of the tail fluke cross-sections with the appropriate...
The values of lift coefficient encountered during manoeuvres13; of a fighter aircraft are known to b...
<p>The lift coefficients (C<sub>L</sub>) and drag coefficients (C<sub>D</sub>) for the bio-realistic...
L3irect[y comparable drag measurements hare been-made of an a ig%oilm“th a conventional rectangular ...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
<p>The proportion of shear drag to drag (D<sub>S</sub>/D) is plotted against angle of attack (α°) fo...
A simple additive correction to the classical representation of the drag coefficient which is insign...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
Averaged lift and drag coeffficients of a DU00-W-212 profile in sinusoidally varying inflow (turbule...
Equations and design charts are given for predicting the downwash angles and the wake characteristic...
Averaged lift and drag coeffficients of a DU00-W-212 profile in laminar flow (background turbulence ...
<p>The lift to drag (L/D) performance of both the bio-realistic (bio) and flat wings plotted against...
Calculated for the cross-sections taken at the base of the tail flukes of the P. phocoena, D. delphi...
Comparison of the chord-normalized profile coordinates of cross-sections taken at the base and top o...
Comparison of the hydrodynamic characteristics of the tail fluke cross-sections with the appropriate...
The values of lift coefficient encountered during manoeuvres13; of a fighter aircraft are known to b...
<p>The lift coefficients (C<sub>L</sub>) and drag coefficients (C<sub>D</sub>) for the bio-realistic...
L3irect[y comparable drag measurements hare been-made of an a ig%oilm“th a conventional rectangular ...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
<p>The proportion of shear drag to drag (D<sub>S</sub>/D) is plotted against angle of attack (α°) fo...
A simple additive correction to the classical representation of the drag coefficient which is insign...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
Averaged lift and drag coeffficients of a DU00-W-212 profile in sinusoidally varying inflow (turbule...
Equations and design charts are given for predicting the downwash angles and the wake characteristic...
Averaged lift and drag coeffficients of a DU00-W-212 profile in laminar flow (background turbulence ...
<p>The lift to drag (L/D) performance of both the bio-realistic (bio) and flat wings plotted against...
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