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An Introduction to Thermodynamic Performance Analysis of Aircraft Gas Turbine Engine Cycles Using the Numerical Propulsion System Simulation Code
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/10/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
Technical Report Jones, Scott M. Glenn Research Center NASA/TM-2007-214690, E-15876 WBS 984754.02.07.03.12.02 JET PROPULSION; GAS TURBINE ENGINES; AIRCRAFT ENGINES; COMPUTER SYSTEMS SIMULATION; COMPUTERIZED SIMULATION; THERMODYNAMIC CYCLES; OBJECT-ORIENTED PROGRAMMING; PROPULSION SYSTEM PERFORMANCE; RELIABILITY ANALYSIS; SYNTAX; PERFORMANCE PREDICTION
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Product Details
ISBN-13:
9798673015544
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
48
Carton Quantity:
85
Product Dimensions:
8.50 x 0.10 x 11.02 inches
Weight:
0.30 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
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Technical Report Jones, Scott M. Glenn Research Center NASA/TM-2007-214690, E-15876 WBS 984754.02.07.03.12.02 JET PROPULSION; GAS TURBINE ENGINES; AIRCRAFT ENGINES; COMPUTER SYSTEMS SIMULATION; COMPUTERIZED SIMULATION; THERMODYNAMIC CYCLES; OBJECT-ORIENTED PROGRAMMING; PROPULSION SYSTEM PERFORMANCE; RELIABILITY ANALYSIS; SYNTAX; PERFORMANCE PREDICTION
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