Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Scientific and Technical Aerospace Reports
Report of the Bureau of Engineering Research
Author: Rutgers University. Bureau of Engineering Research
Publisher:
ISBN:
Category :
Languages : en
Pages : 562
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 562
Book Description
Energy Research Abstracts
Dissertation Abstracts International
Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 1090
Book Description
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 1090
Book Description
Report
Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 844
Book Description
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 844
Book Description
Technical Abstract Bulletin
Fossil Energy Update
NBS Special Publication
Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 264
Book Description
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 264
Book Description
Liquid Propellant Rocket Combustion Instability
Author: David T. Harrje
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 668
Book Description
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 668
Book Description
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.