Author: Robert W. Graham
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 36
Book Description
Energy thickness in prediction of throat heat transfer in rocket nozzles using nozzle geometries and temperature ratios.
The Use of Energy Thickness in Prediction of Throat Heat Transfer in Rocket Nozzles
Author: Robert W. Graham
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 36
Book Description
Energy thickness in prediction of throat heat transfer in rocket nozzles using nozzle geometries and temperature ratios.
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 36
Book Description
Energy thickness in prediction of throat heat transfer in rocket nozzles using nozzle geometries and temperature ratios.
NASA Technical Note
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
Book Description
Monthly Catalog of United States Government Publications
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Applied Mechanics Reviews
Prediction of Local and Integrated Heat Transfer in Nozzles Using an Integral Turbulent Boundary Layer
Author: Donald R. Boldman
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 36
Book Description
An empirical modification of an existing integral energy turbulent boundary layer method is proposed in order to improve the estimates of local heat transfer in converging-diverging nozzles and consequently, provide better assessments of the total or integrated heat transfer. The method involves the use of a modified momentum-heat analogy which includes an acceleration term comprising the nozzle geometry and free stream velocity. The original and modified theories are applied to heat transfer data from previous studies which used heated air in 30 deg - 15 deg, 45 deg - 15 deg, and 60 deg - 15 deg water-cooled nozzles.
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 36
Book Description
An empirical modification of an existing integral energy turbulent boundary layer method is proposed in order to improve the estimates of local heat transfer in converging-diverging nozzles and consequently, provide better assessments of the total or integrated heat transfer. The method involves the use of a modified momentum-heat analogy which includes an acceleration term comprising the nozzle geometry and free stream velocity. The original and modified theories are applied to heat transfer data from previous studies which used heated air in 30 deg - 15 deg, 45 deg - 15 deg, and 60 deg - 15 deg water-cooled nozzles.