IL66077A0 - Leading edge flap for an airfoil - Google Patents

Leading edge flap for an airfoil

Info

Publication number
IL66077A0
IL66077A0 IL66077A IL6607782A IL66077A0 IL 66077 A0 IL66077 A0 IL 66077A0 IL 66077 A IL66077 A IL 66077A IL 6607782 A IL6607782 A IL 6607782A IL 66077 A0 IL66077 A0 IL 66077A0
Authority
IL
Israel
Prior art keywords
airfoil
leading edge
edge flap
flap
leading
Prior art date
Application number
IL66077A
Original Assignee
Lockheed Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US06/274,851 external-priority patent/US4398688A/en
Application filed by Lockheed Corp filed Critical Lockheed Corp
Priority to IL66077A priority Critical patent/IL66077A0/en
Publication of IL66077A0 publication Critical patent/IL66077A0/en

Links

IL66077A 1981-06-18 1982-06-17 Leading edge flap for an airfoil IL66077A0 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IL66077A IL66077A0 (en) 1981-06-18 1982-06-17 Leading edge flap for an airfoil

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/274,851 US4398688A (en) 1979-12-26 1981-06-18 Leading edge flap for an airfoil
IL66077A IL66077A0 (en) 1981-06-18 1982-06-17 Leading edge flap for an airfoil

Publications (1)

Publication Number Publication Date
IL66077A0 true IL66077A0 (en) 1982-09-30

Family

ID=26321051

Family Applications (1)

Application Number Title Priority Date Filing Date
IL66077A IL66077A0 (en) 1981-06-18 1982-06-17 Leading edge flap for an airfoil

Country Status (1)

Country Link
IL (1) IL66077A0 (en)

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