BIBLIO is the largest independent book marketplace in the world, with over 100 million books.

Skip to content

Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor

Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor

Software for calculating the performance of a turboprop engine: Application to
Stock photo: cover may vary

Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor Paperback - 2020

by KANTA, Abdoul-Fatah

Add to wish list
  • Used
  • Good
  • Paperback
Used - Good

Description

paperback. Good. Access codes and supplements are not guaranteed with used items. May be an ex-library book.
Ask the seller a question Add to wish list
A$104.56
Free Delivery within USA
Standard delivery: 7 to 14 days
More delivery options
Dropship order
Ships from Bonita (California, United States)

Details

  • Title Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor
  • Author KANTA, Abdoul-Fatah
  • Binding Paperback
  • Condition Used - Good
  • Pages 108
  • Volumes 1
  • Language ENG
  • Publisher Sciencia Scripts
  • Publication date 2020-07-16
  • Bookseller's Inventory # 6200946728.G
  • ISBN 9786200946720 / 6200946728
  • Weight 0.37 lbs (0.17 kg)
  • Dimensions 9 x 6 x 0.26 in (22.86 x 15.24 x 0.66 cm)
  • Category Technology & Industrial Arts
  • Quantity available 1

About Bonita California, United States

Biblio member since 2020

Terms of Sale: 30 day return guarantee, with full refund including original shipping costs for up to 30 days after delivery if an item arrives misdescribed or damaged.

Browse books from Bonita

Reader reviews for Software for calculating the performance of a turboprop engine: Application to the DART 536-7R reactor

From the publisher

Thrusters play a crucial role in the evolution of aircraft through the different phases of flight. This has led manufacturers to improve engine power in order to bring more efficient products to market that are both quieter and less polluting.In our study, we have developed a calculation code to study the performance of a turboprop engine according to the real cycle and also in non-adaptive mode.The engine will have to operate in a wide range of conditions in terms of Mach number, altitude and rpm. The geometry will then impose, apart from adaptation, constraints which do not exist at the level of the calculation of the initial cycle.The DART 536-7R engine was used as a reference for the application of the developed code.
tracking-