FR911287A - Aile souple à amortissement compensé - Google Patents

Aile souple à amortissement compensé

Info

Publication number
FR911287A
FR911287A FR911287DA FR911287A FR 911287 A FR911287 A FR 911287A FR 911287D A FR911287D A FR 911287DA FR 911287 A FR911287 A FR 911287A
Authority
FR
France
Prior art keywords
soft wing
compensated damping
compensated
damping
wing
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
English (en)
Inventor
Charles Deborne
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
Application filed filed Critical
Application granted granted Critical
Publication of FR911287A publication Critical patent/FR911287A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR911287D 1945-01-09 1945-01-09 Aile souple à amortissement compensé Expired FR911287A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR911287T 1945-01-09

Publications (1)

Publication Number Publication Date
FR911287A true FR911287A (fr) 1946-07-03

Family

ID=9418069

Family Applications (1)

Application Number Title Priority Date Filing Date
FR911287D Expired FR911287A (fr) 1945-01-09 1945-01-09 Aile souple à amortissement compensé

Country Status (1)

Country Link
FR (1) FR911287A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1020871B (de) * 1956-03-16 1957-12-12 Hermann Rosoli Flugzeug mit elastisch an den Flugzeugrumpf angelenkten Schlagfluegeln
US5224665A (en) * 1991-06-10 1993-07-06 General Dynamics Corporation, Convair Division Split span vee tail control arrangement for air vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1020871B (de) * 1956-03-16 1957-12-12 Hermann Rosoli Flugzeug mit elastisch an den Flugzeugrumpf angelenkten Schlagfluegeln
US5224665A (en) * 1991-06-10 1993-07-06 General Dynamics Corporation, Convair Division Split span vee tail control arrangement for air vehicle

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