SE381016B - INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE - Google Patents

INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE

Info

Publication number
SE381016B
SE381016B SE7306302A SE7306302A SE381016B SE 381016 B SE381016 B SE 381016B SE 7306302 A SE7306302 A SE 7306302A SE 7306302 A SE7306302 A SE 7306302A SE 381016 B SE381016 B SE 381016B
Authority
SE
Sweden
Prior art keywords
wing
aircraft
nos
vehicle
geometric location
Prior art date
Application number
SE7306302A
Other languages
Swedish (sv)
Inventor
S E Larson
Original Assignee
S E Larson
Larson I H
Larson C I K
Larson B E H
Larson J E G
Larson L O A
Larson G P G
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 S E Larson, Larson I H, Larson C I K, Larson B E H, Larson J E G, Larson L O A, Larson G P G filed Critical S E Larson
Priority to SE7306302A priority Critical patent/SE381016B/en
Priority to GB1896974A priority patent/GB1470718A/en
Priority to CA198,977A priority patent/CA1005041A/en
Priority to DE2421524A priority patent/DE2421524A1/en
Priority to NL7405987A priority patent/NL7405987A/xx
Priority to FR7415418A priority patent/FR2227991B1/fr
Priority to JP49050208A priority patent/JPS5030299A/ja
Publication of SE381016B publication Critical patent/SE381016B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
SE7306302A 1973-05-04 1973-05-04 INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE SE381016B (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
SE7306302A SE381016B (en) 1973-05-04 1973-05-04 INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE
GB1896974A GB1470718A (en) 1973-05-04 1974-04-30 Vehicle provided with a drag reducing low nose wing
CA198,977A CA1005041A (en) 1973-05-04 1974-05-01 Vehicle provided with a drag reducing low nose wing
DE2421524A DE2421524A1 (en) 1973-05-04 1974-05-03 VEHICLE WITH A RESISTANCE REDUCING LOW DUCK TAIL
NL7405987A NL7405987A (en) 1973-05-04 1974-05-03
FR7415418A FR2227991B1 (en) 1973-05-04 1974-05-03
JP49050208A JPS5030299A (en) 1973-05-04 1974-05-04

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7306302A SE381016B (en) 1973-05-04 1973-05-04 INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE

Publications (1)

Publication Number Publication Date
SE381016B true SE381016B (en) 1975-11-24

Family

ID=20317371

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7306302A SE381016B (en) 1973-05-04 1973-05-04 INCLUDES GEOMETRIC LOCATION OF NOS WING AND MAIN WING AT AIRCRAFT OR OTHER VEHICLE

Country Status (7)

Country Link
JP (1) JPS5030299A (en)
CA (1) CA1005041A (en)
DE (1) DE2421524A1 (en)
FR (1) FR2227991B1 (en)
GB (1) GB1470718A (en)
NL (1) NL7405987A (en)
SE (1) SE381016B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS49134732U (en) * 1973-03-20 1974-11-20
IT1235222B (en) * 1982-11-26 1992-06-26 Secratary Of State For Defence IMPROVEMENT IN MISSILE AND SIMILAR FUSELETS
USRE35387E (en) * 1985-04-09 1996-12-03 Dynamic Engineering, Inc. Superfragile tactical fighter aircraft and method of flying it in supernormal flight
ES9100002A1 (en) * 1985-04-09 1991-01-01 Dynamic Eng Inc Super Agile aircraft and method of flying it in supernormal flight.
DE4337850A1 (en) * 1993-11-05 1995-05-18 Fritz Hausser Rudder, aileron and elevator for front of aircraft
US5901925A (en) * 1996-08-28 1999-05-11 Administrator, National Aeronautics And Space Administration Serrated-planform lifting-surfaces
CN1323900C (en) * 2003-08-22 2007-07-04 中国计量学院 Hydrofoil diving military miniature speedboat and using method thereof
KR100869633B1 (en) * 2007-02-20 2008-11-21 이희성 Tandem/Canard WIG boat
CN113562160B (en) * 2021-08-07 2024-01-02 中国航空工业集团公司沈阳飞机设计研究所 Front wing application method for improving pitching moment characteristics of airplane

Also Published As

Publication number Publication date
FR2227991A1 (en) 1974-11-29
GB1470718A (en) 1977-04-21
JPS5030299A (en) 1975-03-26
NL7405987A (en) 1974-11-06
CA1005041A (en) 1977-02-08
DE2421524A1 (en) 1974-11-21
FR2227991B1 (en) 1980-04-11

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