Textbook of Aero Engines
Textbook of Aero Engines
has 390 pages
Issued date 1920
TABLE OF CONTENTS:
I- Equation of Condition of Gases
II- The Behavior of Combustible Gases During Ignition
III- The Gaseous Mixture
IV- Technical Analysis of the Four Stroke
V- The Work Available and Efficiency
VI- Method of Calculating the Power of and Engine
VII- The Power Variables
VIII- Characteristic Performance
IX- The Effect of Altitude on Power
X- Variation of Power with Pressure
XI- Variation of the Power with the Mixture
XII- The Effect of Increasing Compression
XIII- Technical Analysis of the Power Required for Flight
XIV- The Power and Weight of Aero Engines
XV- General Theory of the Turbo Compressor
XVI- Sherbondy Turbo-Compressor for a 400HP Engine
XVII- Technical Theory of a Turbo Compressor for 400HP Engine
XVIII- The Strength of Rotating Parts of a Turbo-Compressor
XIX- Analysis of Stresses in the Blower Impeller
XX- Study of a Gear Driven Centrifugal
XXI- The Effect of Back Pressure in the Exhaust Manifold on the Power of Engines
XXII- Effect of Altitude on Fuel Economy
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