Author: Lawrence Steve JurewiczPublisher:
ISBN:
Category : Heat
Languages : en
Pages : 166
Book Description
Transpiration Cooling of a Cylinder in Cross Flow with Helium Injection
Author: Lawrence Steve JurewiczPublisher:
ISBN:
Category : Heat
Languages : en
Pages : 166
Book Description
Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow
Author: Richard L. HumphreyPublisher:
ISBN:
Category : Cooling
Languages : en
Pages : 60
Book Description
Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).
Experimental Results of Cooling a 12.5 ̊semivertex Angle Cone by Ejection of Hydrogen and Helium from Its Apex at Mach 7
Author: George F. KlichPublisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 48
Book Description
NASA Technical Note
Author: Journal of Heat Transfer
Author: Analysis Of Heat And Mass Transfer
Author: ECKERTPublisher: CRC Press
ISBN: 9781560326885
Category : Science
Languages : en
Pages : 836
Book Description
Heat Transfer in Aerospace Applications
Author: Bengt SundénPublisher: Academic Press
ISBN: 0128097612
Category : Technology & Engineering
Languages : en
Pages : 274
Book Description
Heat Transfer in Aerospace Applications is the first book to provide an overall description of various heat transfer issues of relevance for aerospace applications. The book contains chapters relating to convection cooling, heat pipes, ablation, heat transfer at high velocity, low pressure and microgravity, aircraft heat exchangers, fuel cells, and cryogenic cooling systems. Chapters specific to low density heat transfer (4) and microgravity heat transfer (9) are newer subjects which have not been previously covered. The book takes a basic engineering approach by including correlations and examples that an engineer needs during the initial phases of vehicle design or to quickly analyze and solve a specific problem. Designed for mechanical, chemical, and aerospace engineers in research institutes, companies, and consulting firms, this book is an invaluable resource for the latest on aerospace heat transfer engineering and research. - Provides an overall description of heat transfer issues of relevance for aerospace applications - Discusses why thermal problems arise and introduces the various heat transfer modes - Helps solve the problem of selecting and calculating the cooling system, the heat exchanger, and heat protection - Features a collection of problems in which the methods presented in the book can be used to solve these problems
A Review of High-speed, Convective, Heat-transfer Computation Methods
Author: Michael E. TauberPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
Transactions of the American Society of Mechanical Engineers
Author: American Society of Mechanical EngineersPublisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 1202
Book Description
Vols. 2, 4-11, 62-68 include the Society's Membership list; v. 55-80 include the Journal of applied mechanics (also issued separately) as contributions from the Society's Applied Mechanics Division.
Author: