The section 24 terminates to form a step 28 that defines a discontinuity in the under surface of the wing between the leading and trailing edges. 2, comprises an extensive main section 24 that extends from along the wing leading edge 26 toward the wing trailing edge. Each wing, taking for example wing 16 and referring now to FIG. 1, are mounted on the fuselage so as to have a small angle-of-attack according to usual practice when the aircraft is on the runway. The airfoils constituting the wings l6 and 18 in FIG. B64C2003/148- Aerofoil profile comprising protuberances, e.g.B64C2003/142- Aerofoil profile with variable camber along the airfoil chord.229910003460 diamond Inorganic materials 0.000 description 1.239000002131 composite material Substances 0.000 description 1.230000003247 decreasing Effects 0.000 claims description 4.Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.) Filing date Publication date Application filed by Richard L Kline, Floyd F Fogleman filed Critical Richard L Kline Priority to US2019570A priority Critical Application granted granted Critical Publication of US3706430A publication Critical patent/US3706430A/en Anticipated expiration legal-status Critical Status Expired - Lifetime legal-status Critical Current Links Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Expired - Lifetime Application number Inventor Richard L Kline Floyd F Fogleman Original Assignee Richard L Kline Floyd F Fogleman Priority date (The priority date is an assumption and is not a legal conclusion.
AIRFOIL TYPES PDF
Google Patents US3706430A - Airfoil for aircraftÄownload PDF Info Publication number US3706430A US3706430A US3706430DA US3706430A US 3706430 A US3706430 A US 3706430A US 3706430D A US3706430D A US 3706430DA US 3706430 A US3706430 A US 3706430A Authority US United States Prior art keywords wing wedge leading edge aircraft airfoil Prior art date Legal status (The legal status is an assumption and is not a legal conclusion.