FR1117244A - Supersonic wind tunnel with variable number of machines - Google Patents
Supersonic wind tunnel with variable number of machinesInfo
- Publication number
- FR1117244A FR1117244A FR1117244DA FR1117244A FR 1117244 A FR1117244 A FR 1117244A FR 1117244D A FR1117244D A FR 1117244DA FR 1117244 A FR1117244 A FR 1117244A
- Authority
- FR
- France
- Prior art keywords
- machines
- wind tunnel
- variable number
- supersonic wind
- supersonic
- 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
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K13/00—Apparatus or processes specially adapted for manufacturing or adjusting assemblages of electric components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
- F15C1/00—Circuit elements having no moving parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/04—Arrangements of guide vanes in pipe elbows or duct bends; Construction of pipe conduit elements for elbows with respect to flow, e.g. for reducing losses of flow
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
- G01M9/04—Details
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Theoretical Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1117244T | 1954-12-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1117244A true FR1117244A (en) | 1956-05-18 |
Family
ID=9629901
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1117244D Expired FR1117244A (en) | 1954-12-20 | 1954-12-20 | Supersonic wind tunnel with variable number of machines |
Country Status (3)
Country | Link |
---|---|
US (1) | US2948148A (en) |
FR (1) | FR1117244A (en) |
GB (1) | GB783046A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3005338A (en) * | 1957-09-23 | 1961-10-24 | Paul A Libby | Nozzle cooling apparatus and method |
CN107741313A (en) * | 2017-11-29 | 2018-02-27 | 中国航空工业集团公司沈阳空气动力研究所 | A kind of low wide Mach number wind-tunnel laminar flow double venturi of disturbance |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3123285A (en) * | 1964-03-03 | Diffuser with boundary layer control | ||
US3212515A (en) * | 1962-07-13 | 1965-10-19 | Giannini Controls Corp | Fluid amplifier |
US3280832A (en) * | 1963-11-18 | 1966-10-25 | Retec Inc | Cycling valve |
FR1463771A (en) * | 1963-12-07 | 1966-07-22 | Snecma | Device for adjusting the flow of fluid in a channel |
US3298599A (en) * | 1964-06-22 | 1967-01-17 | Cons Vacuum Corp | Pump nozzle |
US3396738A (en) * | 1964-11-27 | 1968-08-13 | American Standard Inc | Fluid guiding method and apparatus |
US3302866A (en) * | 1965-03-16 | 1967-02-07 | Polytechnic Inst Brooklyn | High velocity fluid accelerator |
US3363545A (en) * | 1966-07-08 | 1968-01-16 | Owens Illinois Inc | Electrical printing apparatus with means to control boundary layer effect |
US3452782A (en) * | 1966-07-08 | 1969-07-01 | Gen Electric | Fluid discharge casing |
GB1259124A (en) * | 1968-12-06 | 1972-01-05 | ||
US3568703A (en) * | 1969-04-07 | 1971-03-09 | Us Army | Supersonic jet engine inlet flueric bypass control |
US3665949A (en) * | 1969-06-27 | 1972-05-30 | Bendix Corp | Gaseous controlled fluidic throttling valve |
US3695290A (en) * | 1970-07-22 | 1972-10-03 | Kenneth R Evans | Noise suppressing device for fluid flow lines |
US4029430A (en) * | 1975-09-02 | 1977-06-14 | Fonda Bonardi Giusto | Short subsonic diffuser for large pressure ratios |
US4033185A (en) * | 1976-05-18 | 1977-07-05 | The United States Of America As Represented By The Secretary Of The Army | Wind-tunnel simulator |
US4515524A (en) * | 1982-09-27 | 1985-05-07 | Allis-Chalmers Corporation | Draft tube for hydraulic turbine |
US4989807A (en) * | 1988-04-07 | 1991-02-05 | Grumman Aerospace Corporation | S-shaped jet engine inlet diffuser |
US5099685A (en) * | 1990-08-09 | 1992-03-31 | The Boeing Company | Boundary layer control diffuser for a wind tunnel or the like |
DE4343009C2 (en) * | 1993-12-16 | 1996-06-13 | Daimler Benz Aerospace Ag | Injection device, in particular for a jet engine |
US5996936A (en) * | 1997-09-29 | 1999-12-07 | General Electric Company | Fluidic throat exhaust nozzle |
US6444033B1 (en) * | 1999-11-12 | 2002-09-03 | Delsys Pharmaceutical Corp. | Article comprising a diffuser with flow control features |
US6336319B1 (en) | 2000-05-26 | 2002-01-08 | General Electric Company | Fluidic nozzle control system |
US8225592B1 (en) * | 2003-06-09 | 2012-07-24 | Florida State University Research Foundation | Microjet noise suppression system for jet engines |
US7967105B2 (en) * | 2006-06-19 | 2011-06-28 | Yen Tuan | Aero-acoustic aviation engine inlet for aggressive noise abatement |
DE102006041955A1 (en) * | 2006-08-30 | 2008-03-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for controlling combustion in a combustion chamber and combustion chamber device |
US20090165864A1 (en) * | 2007-12-26 | 2009-07-02 | Rolls-Royce North American Technologies, Inc. | Supersonic inlet |
RU2422193C2 (en) | 2009-09-30 | 2011-06-27 | Фисоник Холдинг Лимитед | Device to prepare water-fuel emulsion |
US8485455B2 (en) * | 2010-11-20 | 2013-07-16 | Fisonic Holding Limited | Supersonic nozzle for boiling liquid |
CN103135624B (en) * | 2012-12-19 | 2015-05-13 | 中国空气动力研究与发展中心高速空气动力研究所 | Method for controlling temporary flush type supersonic velocity wind tunnel with ejector function |
CN103954424B (en) * | 2014-04-30 | 2016-05-04 | 北京大学 | Expand method and the hypersonic nozzle in hypersonic quiet jet pipe static test district |
CN104316287B (en) * | 2014-10-24 | 2017-01-11 | 中国人民解放军国防科学技术大学 | Two-dimensional variable-mach-number spray pipe and supersonic-velocity variable-mach-number wind tunnel using same |
KR101909595B1 (en) * | 2017-04-28 | 2018-12-19 | 두산중공업 주식회사 | Exhaust Diffuser Having Spray Hole And Suction Hole, And Gas Turbine Having The Same |
CN109827737B (en) * | 2017-11-23 | 2023-08-11 | 成都凯天电子股份有限公司 | Variable outlet synthetic jet actuator |
CN107806977B (en) * | 2017-11-29 | 2024-04-09 | 中国航空工业集团公司沈阳空气动力研究所 | Combined wide Mach number high enthalpy pulse wind tunnel tube structure |
CN113959674B (en) * | 2021-10-27 | 2023-07-07 | 中国航发沈阳发动机研究所 | Rectangular wind tunnel end wall surface layer sucking structure |
CN114061891B (en) * | 2022-01-18 | 2022-03-29 | 中国空气动力研究与发展中心高速空气动力研究所 | Downward-blowing injection type static pressure matching control method for large-size open jet wind tunnel |
CN114061890B (en) * | 2022-01-18 | 2022-03-29 | 中国空气动力研究与发展中心高速空气动力研究所 | Downward blowing type static pressure matching control method for large-size opening jet flow wind tunnel |
CN114608792B (en) * | 2022-05-10 | 2022-07-15 | 中国空气动力研究与发展中心高速空气动力研究所 | Method for measuring uniform region of sub-transonic jet flow field of high-speed jet wind tunnel by short-shaft probe |
CN116358825A (en) * | 2023-05-26 | 2023-06-30 | 中国航空工业集团公司沈阳空气动力研究所 | Continuous wind tunnel Mach number fine adjustment mechanism and adjustment method |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB616163A (en) * | 1943-01-19 | 1949-01-18 | Groupement Francais Pour Le Developpement Des Recherches Aeronautiques | Means for avoid separation and turbulence in fluids moving with respect to solid surfaces |
US2729974A (en) * | 1952-02-15 | 1956-01-10 | United Aircraft Corp | Transonic flow control with reduced power |
US2678560A (en) * | 1952-10-09 | 1954-05-18 | Us Navy | Supersonic wind tunnel |
US2788719A (en) * | 1954-02-11 | 1957-04-16 | Klmberly Clark Corp | Flow control apparatus |
-
1954
- 1954-12-20 FR FR1117244D patent/FR1117244A/en not_active Expired
-
1955
- 1955-12-15 GB GB36050/55A patent/GB783046A/en not_active Expired
- 1955-12-20 US US554358A patent/US2948148A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3005338A (en) * | 1957-09-23 | 1961-10-24 | Paul A Libby | Nozzle cooling apparatus and method |
CN107741313A (en) * | 2017-11-29 | 2018-02-27 | 中国航空工业集团公司沈阳空气动力研究所 | A kind of low wide Mach number wind-tunnel laminar flow double venturi of disturbance |
Also Published As
Publication number | Publication date |
---|---|
US2948148A (en) | 1960-08-09 |
GB783046A (en) | 1957-09-18 |
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