CH326600A - Method for adjusting the flow velocity of a gas in a supersonic blower nozzle and nozzle for carrying out this method - Google Patents

Method for adjusting the flow velocity of a gas in a supersonic blower nozzle and nozzle for carrying out this method

Info

Publication number
CH326600A
CH326600A CH326600DA CH326600A CH 326600 A CH326600 A CH 326600A CH 326600D A CH326600D A CH 326600DA CH 326600 A CH326600 A CH 326600A
Authority
CH
Switzerland
Prior art keywords
nozzle
supersonic
adjusting
carrying
gas
Prior art date
Application number
Other languages
French (fr)
Inventor
Menard Maurice
Original Assignee
Conservatoire Nat Arts
Menard Maurice
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 Conservatoire Nat Arts, Menard Maurice filed Critical Conservatoire Nat Arts
Publication of CH326600A publication Critical patent/CH326600A/en

Links

Classifications

    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
CH326600D 1951-06-29 1952-02-07 Method for adjusting the flow velocity of a gas in a supersonic blower nozzle and nozzle for carrying out this method CH326600A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR326600X 1951-06-29

Publications (1)

Publication Number Publication Date
CH326600A true CH326600A (en) 1957-12-31

Family

ID=8890559

Family Applications (1)

Application Number Title Priority Date Filing Date
CH326600D CH326600A (en) 1951-06-29 1952-02-07 Method for adjusting the flow velocity of a gas in a supersonic blower nozzle and nozzle for carrying out this method

Country Status (2)

Country Link
US (1) US2831505A (en)
CH (1) CH326600A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104680A (en) * 1962-01-19 1963-09-24 William J Orlin Supersonic nozzle
US3461833A (en) * 1966-12-27 1969-08-19 Bendix Corp Fluid variable pressure device
CH572190A5 (en) * 1973-11-23 1976-01-30 Sulzer Ag
US4398415A (en) * 1981-12-10 1983-08-16 The United States Of America As Represented By The Secretary Of The Air Force Swing link flexible wind tunnel nozzle
US4678396A (en) * 1982-11-04 1987-07-07 A S Kongsberg Vapenfabrikk Movable spike, variable entrance geometry pipe diffuser with vibration suppression

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2229819A (en) * 1937-11-04 1941-01-28 Packard Motor Car Co Carburetor
US2582814A (en) * 1947-07-31 1952-01-15 Lockheed Aircraft Corp Transonic wind tunnel
FR969291A (en) * 1948-07-09 1950-12-18 Matemine Sa Adjustable pressure relief nozzle for flow of compressible fluids

Also Published As

Publication number Publication date
US2831505A (en) 1958-04-22

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