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AU2001232661A1 - Passive aerodynamic sonic boom suppression for supersonic aircraft - Google Patents

Passive aerodynamic sonic boom suppression for supersonic aircraft

Info

Publication number
AU2001232661A1
AU2001232661A1 AU2001232661A AU3266101A AU2001232661A1 AU 2001232661 A1 AU2001232661 A1 AU 2001232661A1 AU 2001232661 A AU2001232661 A AU 2001232661A AU 3266101 A AU3266101 A AU 3266101A AU 2001232661 A1 AU2001232661 A1 AU 2001232661A1
Authority
AU
Australia
Prior art keywords
supersonic aircraft
sonic boom
passive aerodynamic
suppression
boom suppression
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.)
Abandoned
Application number
AU2001232661A
Inventor
Tom Hartmann
John M. Morgenstern
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of AU2001232661A1 publication Critical patent/AU2001232661A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/04—Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
AU2001232661A 2000-02-08 2000-12-22 Passive aerodynamic sonic boom suppression for supersonic aircraft Abandoned AU2001232661A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09499654 2000-02-08
US09/499,654 US6588703B1 (en) 2000-02-08 2000-02-08 Passive aerodynamic sonic boom suppression for supersonic aircraft
PCT/US2000/035148 WO2001058754A1 (en) 2000-02-08 2000-12-22 Passive aerodynamic sonic boom suppression for supersonic aircraft

Publications (1)

Publication Number Publication Date
AU2001232661A1 true AU2001232661A1 (en) 2001-08-20

Family

ID=23986132

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001232661A Abandoned AU2001232661A1 (en) 2000-02-08 2000-12-22 Passive aerodynamic sonic boom suppression for supersonic aircraft

Country Status (7)

Country Link
US (1) US6588703B1 (en)
EP (1) EP1254048A1 (en)
JP (1) JP2003522076A (en)
KR (1) KR20020079835A (en)
AU (1) AU2001232661A1 (en)
CA (1) CA2398528A1 (en)
WO (1) WO2001058754A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0315431D0 (en) * 2003-07-02 2003-08-06 Rolls Royce Plc Aircraft configuration
WO2005047102A2 (en) * 2003-11-11 2005-05-26 Supersonic Aerospace International Llc Systems and methods for configuring aircraft to meet performance goals and shock wave disturbance constraints
WO2005062743A2 (en) 2003-10-30 2005-07-14 Supersonic Aerospace International, Llc Supersonic aircraft with aerodynamic tail structure
US6854687B1 (en) * 2003-11-11 2005-02-15 Supersonic Aerospace International, Inc. Nacelle integration with reflexed wing for sonic boom reduction
US8473254B2 (en) * 2003-11-14 2013-06-25 Supersonic Aerospace International, Llc Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints
US7118071B2 (en) * 2004-03-31 2006-10-10 The Boeing Company Methods and systems for controlling lower surface shocks
US20060038063A1 (en) * 2004-08-18 2006-02-23 Northrop Grumman Corporation Shaped sonic boom aircraft
JP5228149B2 (en) * 2007-11-15 2013-07-03 国立大学法人豊橋技術科学大学 Nozzle for film formation, film formation method, and film formation member
US8646373B1 (en) 2009-05-04 2014-02-11 Nova Research, Inc. Blast wave effects reduction system
US8453974B1 (en) * 2010-12-13 2013-06-04 The Boeing Company Flow channels
US10093410B2 (en) * 2013-02-14 2018-10-09 Gulfstream Aerospace Corporation Systems and methods for controlling a magnitude of a sonic boom
US10618638B2 (en) 2015-09-22 2020-04-14 Nctar, Llc Shockwave mitigation system for supersonic aircraft
CN110550203A (en) * 2019-09-03 2019-12-10 中国航空工业集团公司西安飞机设计研究所 Supersonic aircraft
CN114435580B (en) * 2022-03-25 2023-02-28 西北工业大学 Generalized silence awl pneumatic layout configuration to supersonic speed civil aircraft

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1786472A (en) * 1928-11-02 1930-12-30 Walter F Woodul Airfoil
US2916230A (en) * 1948-01-14 1959-12-08 Gen Electric Supersonic airfoil
US3137460A (en) * 1957-11-01 1964-06-16 North American Aviation Inc Improving supersonic lift-to-drag ratio by compression shock
US3677502A (en) * 1969-03-10 1972-07-18 Andrei Nikolaevich Tupolev Supersonic aircraft
US4114836A (en) * 1977-03-09 1978-09-19 Blair M. Graham Airplane configuration designed for the simultaneous reduction of drag and sonic boom
US4598886A (en) * 1979-08-13 1986-07-08 The Boeing Company Double parasol, favorable interference airplane
US4436261A (en) 1980-04-23 1984-03-13 Kolio Koleff V/STOL Aircraft
US4582276A (en) 1981-12-28 1986-04-15 Northrop Corporation Lifting shock wave cancellation module
US4867394A (en) 1988-06-23 1989-09-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Compression pylon
US5322242A (en) 1991-07-08 1994-06-21 Tracy Richard R High efficiency, supersonic aircraft
US5529263A (en) * 1992-10-21 1996-06-25 The Boeing Company Supersonic airplane with subsonic boost engine means and method of operating the same
US5289995A (en) 1992-12-14 1994-03-01 The Boeing Company Supersonic aircraft
US5443230A (en) 1993-12-21 1995-08-22 United Technologies Corporation Aircraft wing/nacelle combination
US5740984A (en) * 1994-09-22 1998-04-21 Mcdonnell Douglas Corporation Low sonic boom shock control/alleviation surface
US5934607A (en) * 1997-01-21 1999-08-10 Lockheed Martin Corporation Shock suppression supersonic aircraft
US5899413A (en) * 1997-12-01 1999-05-04 Mcdonnell Douglas Corporation Non-waisted fuselage design for supersonic aircraft

Also Published As

Publication number Publication date
EP1254048A1 (en) 2002-11-06
KR20020079835A (en) 2002-10-19
US6588703B1 (en) 2003-07-08
WO2001058754A1 (en) 2001-08-16
CA2398528A1 (en) 2001-08-16
JP2003522076A (en) 2003-07-22

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