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Source: The Open Library

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1Shock-tunnel combustor testing for hypersonic vehicles

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“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:

  • Title: ➤  Shock-tunnel combustor testing for hypersonic vehicles
  • Author:
  • Language: English
  • Publisher: ➤  MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - San Jose, Calif - [Washington, DC

“Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1994
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    2An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications

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    “An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” Metadata:

    • Title: ➤  An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

    “An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1986
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications at online marketplaces:



      Wiki

      Source: Wikipedia

      Wikipedia Results

      Search Results from Wikipedia

      De Laval nozzle

      switched to a converging-diverging nozzle in his steam jet pumps by 1878 after using convergent nozzles but these nozzles remained a company secret. In 1888

      Surface effect ship

      on by air or sea, and it can use water jets for propulsion since the inlet nozzles are always covered by water. The United States Navy initiated the SES

      Components of jet engines

      intake (inlet) — For subsonic aircraft, the inlet is a duct which is required to ensure smooth airflow into the engine despite air approaching the inlet from

      Compressible flow

      applications such as: aircraft inlet design, objects in supersonic flight, and (at a more fundamental level) supersonic nozzles and diffusers. Depending on

      Metropolitan-Vickers F.2

      combustion chamber, which caused warping and fracturing of the turbine inlet nozzles. Around seven weeks after its first flight, on 4th January 1944, DG204/G

      Rocket engine nozzle

      Controlled flow-separation nozzles include: expanding nozzle, bell nozzles with a removable insert, stepped nozzles, or dual-bell nozzles. These are generally

      Rotodynamic pump

      the inlet nozzle (at the suction) is empty or filled with the air it will damage the impeller. The difference between pressure created at the inlet nozzle

      Lockheed SR-71 Blackbird

      60086 711 8, p. 328. "Variable Area Exhaust Nozzle", U.S. Patent 3,062,003 "Variable Geometry Exhaust Nozzles and Their Effects on Airplane Performance"

      Turbofan

      Turbofan engine noise propagates both upstream via the inlet and downstream via the primary nozzle and the by-pass duct. Other noise sources are the fan

      Combustor

      Astronautics. ISBN 1-56347-538-3. Mattingly, Jack D. (2006). "Chapter 10: Inlets, Nozzles, and Combustion Systems". Elements of Propulsion: Gas Turbines and