IT995688B - Ala supersonica a flusso ascendente - Google Patents

Ala supersonica a flusso ascendente

Info

Publication number
IT995688B
IT995688B IT29883/73A IT2988373A IT995688B IT 995688 B IT995688 B IT 995688B IT 29883/73 A IT29883/73 A IT 29883/73A IT 2988373 A IT2988373 A IT 2988373A IT 995688 B IT995688 B IT 995688B
Authority
IT
Italy
Prior art keywords
ascending flow
supersonic wing
supersonic
wing
ascending
Prior art date
Application number
IT29883/73A
Other languages
English (en)
Original Assignee
Rethorst Scott Carson
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 Rethorst Scott Carson filed Critical Rethorst Scott Carson
Application granted granted Critical
Publication of IT995688B publication Critical patent/IT995688B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • 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)
  • Toys (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT29883/73A 1973-03-16 1973-10-09 Ala supersonica a flusso ascendente IT995688B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US342151A US3904151A (en) 1973-03-16 1973-03-16 Supersonic upflow wing

Publications (1)

Publication Number Publication Date
IT995688B true IT995688B (it) 1975-11-20

Family

ID=23340576

Family Applications (1)

Application Number Title Priority Date Filing Date
IT29883/73A IT995688B (it) 1973-03-16 1973-10-09 Ala supersonica a flusso ascendente

Country Status (6)

Country Link
US (1) US3904151A (it)
JP (1) JPS5047399A (it)
DE (1) DE2412069A1 (it)
FR (1) FR2323577A1 (it)
GB (1) GB1441646A (it)
IT (1) IT995688B (it)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4008866A (en) * 1973-03-16 1977-02-22 Vehicle Research Corporation Compression energy transformation system for a supersonic wing
US4168044A (en) * 1975-06-06 1979-09-18 Vehicle Research Corporation Energy conserving supersonic aircraft
WO1992001602A1 (en) * 1990-07-23 1992-02-06 Vehicle Research Corporation Supersonic aircraft shock wave energy recovery system
US5251846A (en) * 1990-07-23 1993-10-12 Vehicle Research Corporation Supersonic aircraft shock wave energy recovery system
US5676333A (en) * 1990-07-23 1997-10-14 Rethorst; Scott Supersonic aircraft shock wave energy recovery system
US5358156A (en) * 1990-07-23 1994-10-25 Vehicle Research Corporation Supersonic aircraft shock wave energy recovery system
US5348256A (en) * 1992-05-13 1994-09-20 The Boeing Company Supersonic aircraft and method
US5634613A (en) * 1994-07-18 1997-06-03 Mccarthy; Peter T. Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect
US5934607A (en) * 1997-01-21 1999-08-10 Lockheed Martin Corporation Shock suppression supersonic aircraft
US6082679A (en) * 1997-06-26 2000-07-04 The Boeing Company Active system for early destruction of trailing vortices
FR2821605B1 (fr) * 2001-03-01 2003-05-30 Eads Airbus Sa Procede et dispositif pour accelerer la destruction d'au moins deux vortex dans le sillage d'un mobile, en particulier d'un avion
US7207526B2 (en) * 2002-06-26 2007-04-24 Mccarthy Peter T High efficiency tip vortex reversal and induced drag reduction
AU2003249321B2 (en) * 2002-07-19 2010-02-18 Peter T. Mccarthy Propulsion hydrofoils
US7861966B2 (en) * 2005-04-18 2011-01-04 Vehicle Research Corporation Supersonic aircraft footprint spreading control system and method
RU2461492C2 (ru) * 2010-11-01 2012-09-20 Джабраил Харунович Базиев Профиль крыла летательного аппарата (варианты)
US8949090B2 (en) * 2013-01-28 2015-02-03 The Boeing Company Formation flight control
US10618638B2 (en) * 2015-09-22 2020-04-14 Nctar, Llc Shockwave mitigation system for supersonic aircraft
EP3309065B1 (de) * 2016-10-11 2020-08-26 Airbus Defence and Space GmbH Verfahren zur beeinflussung von querstrominstabilitäten an einem strömungskörper sowie strömungskörpersystem
US11299255B2 (en) * 2016-12-12 2022-04-12 Bombardier Inc. Aircraft slat including angled outboard edge
CN114906316A (zh) * 2022-04-15 2022-08-16 西华大学 超声速吹气环量后缘装置和飞行器
WO2024243337A2 (en) * 2023-05-22 2024-11-28 Arizona Board Of Regents On Behalf Of The University Of Arizona Supersonic jet curtains for control of moments and forces on aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2891740A (en) * 1957-06-27 1959-06-23 John P Campbell External-flow jet flap
FR1372548A (fr) * 1963-07-30 1964-09-18 English Electric Co Ltd Aile d'avion supersonique
US3314629A (en) * 1964-12-07 1967-04-18 Scott C Rethorst Shockless supersonic aircraft
FR1558295A (it) * 1967-06-27 1969-02-28
US3612446A (en) * 1969-10-10 1971-10-12 Herbert A Lebert Means and method for preventing the formation of audible frequencies in fluids passing over an airfoil section
US3737119A (en) * 1970-06-15 1973-06-05 Research Corp Device for sonic boom reduction and improving aircraft performance

Also Published As

Publication number Publication date
GB1441646A (en) 1976-07-07
DE2412069A1 (de) 1974-09-19
US3904151A (en) 1975-09-09
FR2323577A1 (fr) 1977-04-08
FR2323577B1 (it) 1983-04-15
JPS5047399A (it) 1975-04-26

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