Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid Blade Configuration

by National Aeronautics and Space Adm Nasa

0 ratings • 0 reviews • 0 shelved
Book cover for Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3
Shelve It

Bookhype may earn a small commission from qualifying purchases. Full disclosure.

  • ISBN10 171995285X
  • ISBN13 9781719952859
  • Publish Date 29 August 2018 (first published 25 August 2018)
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 28
  • Language English