A Study of the Effect of Aftercooling on the Power and the Weight of a 2000-Horsepower Air-Cooled Engine Installation

Abstract

Investigations were made to determine effects of aftercooling on brake horsepower and weight power ratio. An increase in bhp of 42% was obtained with superchargers operating at constant manifold temperature and aftercooling to a manifold temperature of 40 deg F. Supercharging to a detonation limited manifold pressure and aftercooling to a temperature of 40 deg F resulted in an increase of 65% in bhp. A 10% reduction in weight-power ratio was produced for a system operating at detonation-limited manifold pressure and aftercooling to a temperature of 80 to 100 deg F.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1944
Accession Number
ADA801394

Entities

People

  • D. E. Brimley
  • George P. Wood

Organizations

  • National Advisory Committee for Aeronautics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Cooled
  • Air Pressure
  • Air Temperature
  • Aircrafts
  • Airplanes
  • Connecting Rods
  • Cooling
  • Detonations
  • Engines
  • Heat Energy
  • Heat Exchangers
  • Heat Transfer
  • Horsepower
  • Induction Systems
  • Superchargers

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.