FR931003A - Avion - Google Patents

Avion

Info

Publication number
FR931003A
FR931003A FR931003DA FR931003A FR 931003 A FR931003 A FR 931003A FR 931003D A FR931003D A FR 931003DA FR 931003 A FR931003 A FR 931003A
Authority
FR
France
Prior art keywords
plane
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
Roger-Aime Robert
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 FR931003A publication Critical patent/FR931003A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR931003D 1946-04-13 1946-04-13 Avion Expired FR931003A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR931003T 1946-04-13

Publications (1)

Publication Number Publication Date
FR931003A true FR931003A (fr) 1948-02-11

Family

ID=9450252

Family Applications (1)

Application Number Title Priority Date Filing Date
FR931003D Expired FR931003A (fr) 1946-04-13 1946-04-13 Avion

Country Status (1)

Country Link
FR (1) FR931003A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2874922A (en) * 1956-08-24 1959-02-24 Richard T Whitcomb Fuselage shaping to reduce the strength of shock waves about airplanes at transonic and supersonic speeds

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2874922A (en) * 1956-08-24 1959-02-24 Richard T Whitcomb Fuselage shaping to reduce the strength of shock waves about airplanes at transonic and supersonic speeds

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