Author: Robert T. Swann
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 56
Book Description
Theoretical Analysis of Effects of Ablation on Heat Transfer to an Arbitrary Axisymmetric Body
Author: Robert T. Swann
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 56
Book Description
NASA Technical Note
An Experimental Investigation of Several Ablation Materials in an Electric-arc-heated Air Jet
Author: Andrew J. Chapman
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Ablation (Aerothermodynamics)
Languages : en
Pages : 48
Book Description
Technical Abstract Bulletin
Astronautics Information Abstracts
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Astronautics Information Abstracts
Author: Jet Propulsion Laboratory (U.S.).
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 336
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 336
Book Description
Numerical Analysis of the Transient Response of Advanced Thermal Protection Systems for Atmospheric Entry
Author: Robert T. Swann
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44
Book Description
Equations for the transfer of heat through thermal protection shields are derived in finite difference form. These equations are applicable to charring ablators, impregnated ceramics, subliming ablators, heat sinks, and insulating materials and have been programmed for solution on a high speed digital computer.
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44
Book Description
Equations for the transfer of heat through thermal protection shields are derived in finite difference form. These equations are applicable to charring ablators, impregnated ceramics, subliming ablators, heat sinks, and insulating materials and have been programmed for solution on a high speed digital computer.
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
Book Description