NL62905C - - Google Patents

Info

Publication number
NL62905C
NL62905C NL62905DA NL62905C NL 62905 C NL62905 C NL 62905C NL 62905D A NL62905D A NL 62905DA NL 62905 C NL62905 C NL 62905C
Authority
NL
Netherlands
Application number
Publication of NL62905C publication Critical patent/NL62905C/xx

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
NL62905D NL62905C (en)

Publications (1)

Publication Number Publication Date
NL62905C true NL62905C (en)

Family

ID=1817440

Family Applications (1)

Application Number Title Priority Date Filing Date
NL62905D NL62905C (en)

Country Status (1)

Country Link
NL (1) NL62905C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2912992A1 (en) * 2007-02-23 2008-08-29 Novac Modoran Supersonic aircraft for executing military mission, has delta wing provided with ailerons and flaps at ends of wing, aerodynamic pressure channel sealingly mounted at compressor, and air intakes provided with rack and pinion drive

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2912992A1 (en) * 2007-02-23 2008-08-29 Novac Modoran Supersonic aircraft for executing military mission, has delta wing provided with ailerons and flaps at ends of wing, aerodynamic pressure channel sealingly mounted at compressor, and air intakes provided with rack and pinion drive

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