We have investigated the maximum lift obtainable with slotted airfoils derived from a symmetrical airfoil. These should have a smaller profile drag than other slotted airfoils.
Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S.T. Ae.) of Rhode St. Genese, Brussels
01.02.1928
Sonstige
Keine Angabe
Englisch
AIRFOILS - RHODE ST GENESE 43B - CHAR & MOMENTS WING SLOTS , AIRLOILS - RHODE ST GENESE 43A - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40C - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40E - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 43C - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40F - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40A - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40B - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40G - CHAR & MOMENTS WING SLOTS , AIRFOILS - RHODE ST GENESE 40D - CHAR & MOMENTS WING SLOTS
Engineering Index Backfile | 1928
|Slotted Airfoils for Increasing the Aerodynamic Efficiency (AIAA 2017-1839)
British Library Conference Proceedings | 2017
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