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
1928-02-01
Miscellaneous
No indication
English
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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