Add to ORKGWard's slender-body-theory formula for zero-lift drag contains three integrals plus a base-drag term...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
One promising application of recent advances in electric aircraft propulsion technologies is a blown...
This study is an extension of our previous work that was conducted on the aerodynamic characteristic...
The perfect wing is a dream that many airplane manufactures have been striving to achieve since the ...
Some of the objectives of modern aircraft development are related to the achievement of reduced fuel...
Results of investigations of several promising methods for alleviating the drag rise of transport co...
The viewgraphs and discussion of high lift system aerodynamic requirements are provided. Low speed a...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
Drag reduction for aerial vehicles has a range of positive ramifications: reduced fuel consumption, ...
The classic minimum induced drag spanload is not necessarily the best choice for an aircraft. For a ...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
Most leading-edge tubercles studies (inspired from the humpback whale) involve serrated-type leading...
Considered apart from its propulsive system the high altitude airplane itself adapted to higher flig...
Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a c...
Ward's slender-body-theory formula for zero-lift drag contains three integrals plus a base-drag term...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
One promising application of recent advances in electric aircraft propulsion technologies is a blown...
This study is an extension of our previous work that was conducted on the aerodynamic characteristic...
The perfect wing is a dream that many airplane manufactures have been striving to achieve since the ...
Some of the objectives of modern aircraft development are related to the achievement of reduced fuel...
Results of investigations of several promising methods for alleviating the drag rise of transport co...
The viewgraphs and discussion of high lift system aerodynamic requirements are provided. Low speed a...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
Drag reduction for aerial vehicles has a range of positive ramifications: reduced fuel consumption, ...
The classic minimum induced drag spanload is not necessarily the best choice for an aircraft. For a ...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
Most leading-edge tubercles studies (inspired from the humpback whale) involve serrated-type leading...
Considered apart from its propulsive system the high altitude airplane itself adapted to higher flig...
Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a c...
Ward's slender-body-theory formula for zero-lift drag contains three integrals plus a base-drag term...
The drag of bodies has now assumed greater importance because, as shown in NACA RM L53I15a, 1953 and...
One promising application of recent advances in electric aircraft propulsion technologies is a blown...