Analysis of Jet-propulsion Engine Combustion-chamber Pressure Losses PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Analysis of Jet-propulsion Engine Combustion-chamber Pressure Losses PDF full book. Access full book title Analysis of Jet-propulsion Engine Combustion-chamber Pressure Losses by I. Irving Pinkel. Download full books in PDF and EPUB format.
Author: I. Irving Pinkel
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 11
Get Book Here
Book Description
The over-all pressure losses computed from the pressure-loss chart are within 7 percent of the experimental values for the three types of combustion chamber presented herein.
Author: I. Irving Pinkel
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 11
Get Book Here
Book Description
The over-all pressure losses computed from the pressure-loss chart are within 7 percent of the experimental values for the three types of combustion chamber presented herein.
Author: Reece V. Hensley
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
Get Book Here
Book Description
Author: I. Irving Pinkel
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Get Book Here
Book Description
Author: Bemrose Boyd
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 46
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 324
Get Book Here
Book Description
Author: Richard P. Krebs
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 900
Get Book Here
Book Description
Author: John F. Darsow
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Get Book Here
Book Description
The thermal performance of an air-heated propeller, installed on a test airplane, was evaluated by observations of the ice-prevention propertiesof the propeller during flight in natural-icing conditions and by the collection of thermal data on the propeller during flight in clear air and in clouds at temperatures above freezing. The test propeller was equipped with hollow steel blades of a standard design which were altered to permit heated air to enter the blade cavities at the propeller hub and to leave the cavities at the blade tips. No provisions were made to control the distribution of air flow inside the blades.
Author: Society of Automotive Engineers
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 628
Get Book Here
Book Description
Author: E. R. Norster
Publisher: Elsevier
ISBN: 1483151794
Category : Technology & Engineering
Languages : en
Pages : 417
Get Book Here
Book Description
Combustion and Heat Transfer in Gas Turbine Systems is a compilation of papers from the Proceedings of an International Propulsion Symposium held at the College of Aeronautics, Cranfield in April 1969. This compilation deals with research done by academic and scientific institutions and of industrial organizations, with some research papers covering atomization, fuels, and high-temperature materials. One paper describes the combustion system of the Concorde engine used in commercial flights, temperature of metal parts, and some design modifications to increase the mechanical life of the combustion system. Another paper discusses the evolution of the RB 162 combustion system that is used in the vertical takeoff and landing aircrafts. The RB 162 has many design features of the earlier single reversal chamber and differs in only one or two points. The book then notes the necessity of a plenum chamber burning to further development of supersonic engines and flight. One paper also proposes an alternative theory to the traditional ignition theory of altitude relighting such as those developed by Lewis and von Elbe. Another paper reposts on some observations made of the atomizing characteristics of air-blast atomizers and proposes simple changes to improve the performance of the atomizer by prefilming and allowing air to both sides of the fuel. This compilation will prove very helpful for aeronautical engineers, aviation designers, physicists, students of engineering, and readers who are interested in the design and development of jet engines and supersonic aircrafts.
