FR929942A - Procédé et dispositifs de contrôle des écoulements transsoniques - Google Patents

Procédé et dispositifs de contrôle des écoulements transsoniques

Info

Publication number
FR929942A
FR929942A FR929942DA FR929942A FR 929942 A FR929942 A FR 929942A FR 929942D A FR929942D A FR 929942DA FR 929942 A FR929942 A FR 929942A
Authority
FR
France
Prior art keywords
controlling
devices
transonic flows
transonic
flows
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)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Original Assignee
Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
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 by Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE filed Critical Societe Nationale des Constructions Aeronautiques du Sud Est SNCASE
Application granted granted Critical
Publication of FR929942A publication Critical patent/FR929942A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR929942D 1946-06-17 1946-06-17 Procédé et dispositifs de contrôle des écoulements transsoniques Expired FR929942A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR929942T 1946-06-17

Publications (1)

Publication Number Publication Date
FR929942A true FR929942A (fr) 1948-01-12

Family

ID=9442773

Family Applications (1)

Application Number Title Priority Date Filing Date
FR929942D Expired FR929942A (fr) 1946-06-17 1946-06-17 Procédé et dispositifs de contrôle des écoulements transsoniques

Country Status (1)

Country Link
FR (1) FR929942A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2730313A (en) * 1952-12-12 1956-01-10 Chance Vought Aircraft Inc Airfoil protuberance for improving spoiler effectiveness
US2739770A (en) * 1952-11-14 1956-03-27 United Aircraft Corp Airfoil anti-flutter device
EP0558904A1 (fr) * 1992-03-06 1993-09-08 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Aile pour avion avec profile supercritique

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2739770A (en) * 1952-11-14 1956-03-27 United Aircraft Corp Airfoil anti-flutter device
US2730313A (en) * 1952-12-12 1956-01-10 Chance Vought Aircraft Inc Airfoil protuberance for improving spoiler effectiveness
EP0558904A1 (fr) * 1992-03-06 1993-09-08 DaimlerChrysler Aerospace Airbus Gesellschaft mit beschränkter Haftung Aile pour avion avec profile supercritique

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