CA1005041A - Vehicle provided with a drag reducing low nose wing - Google Patents
Vehicle provided with a drag reducing low nose wingInfo
- Publication number
- CA1005041A CA1005041A CA198,977A CA198977A CA1005041A CA 1005041 A CA1005041 A CA 1005041A CA 198977 A CA198977 A CA 198977A CA 1005041 A CA1005041 A CA 1005041A
- Authority
- CA
- Canada
- Prior art keywords
- vehicle provided
- drag reducing
- reducing low
- nose wing
- low nose
- 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
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)
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 |
|---|---|
| CA1005041A true CA1005041A (en) | 1977-02-08 |
Family
ID=20317371
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA198,977A Expired CA1005041A (en) | 1973-05-04 | 1974-05-01 | Vehicle provided with a drag reducing low nose wing |
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 (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS49134732U (en) * | 1973-03-20 | 1974-11-20 | ||
| US4428549A (en) | 1980-10-24 | 1984-01-31 | British Aerospace Public Limited Company | Arrangements for mounting a probe on an aircraft |
| IT1235222B (en) * | 1982-11-26 | 1992-06-26 | Secratary Of State For Defence | IMPROVEMENT IN MISSILE AND SIMILAR FUSELETS |
| ES9100002A1 (en) * | 1985-04-09 | 1991-01-01 | Dynamic Eng Inc | Super Agile aircraft and method of flying it in supernormal flight. |
| USRE35387E (en) * | 1985-04-09 | 1996-12-03 | Dynamic Engineering, Inc. | Superfragile tactical fighter 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 Wigs |
| 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 |
-
1973
- 1973-05-04 SE SE7306302A patent/SE381016B/en unknown
-
1974
- 1974-04-30 GB GB1896974A patent/GB1470718A/en not_active Expired
- 1974-05-01 CA CA198,977A patent/CA1005041A/en not_active Expired
- 1974-05-03 NL NL7405987A patent/NL7405987A/xx unknown
- 1974-05-03 DE DE2421524A patent/DE2421524A1/en not_active Withdrawn
- 1974-05-03 FR FR7415418A patent/FR2227991B1/fr not_active Expired
- 1974-05-04 JP JP49050208A patent/JPS5030299A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| NL7405987A (en) | 1974-11-06 |
| DE2421524A1 (en) | 1974-11-21 |
| SE381016B (en) | 1975-11-24 |
| GB1470718A (en) | 1977-04-21 |
| JPS5030299A (en) | 1975-03-26 |
| FR2227991B1 (en) | 1980-04-11 |
| FR2227991A1 (en) | 1974-11-29 |
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