BE400219A - - Google Patents

Info

Publication number
BE400219A
BE400219A BE400219DA BE400219A BE 400219 A BE400219 A BE 400219A BE 400219D A BE400219D A BE 400219DA BE 400219 A BE400219 A BE 400219A
Authority
BE
Belgium
Prior art keywords
airplane
groove
tapered surface
aircraft
hull
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE400219A publication Critical patent/BE400219A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
BE400219D BE400219A (en:Method)

Publications (1)

Publication Number Publication Date
BE400219A true BE400219A (en:Method)

Family

ID=66379

Family Applications (1)

Application Number Title Priority Date Filing Date
BE400219D BE400219A (en:Method)

Country Status (1)

Country Link
BE (1) BE400219A (en:Method)

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