Analysis of the Transient Radiation Heat Transfer of an Uncooled Rocket Engine Operating Outside Earth's Atmosphere 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 the Transient Radiation Heat Transfer of an Uncooled Rocket Engine Operating Outside Earth's Atmosphere PDF full book. Access full book title Analysis of the Transient Radiation Heat Transfer of an Uncooled Rocket Engine Operating Outside Earth's Atmosphere by William H. Robbins. Download full books in PDF and EPUB format.
Author: William H. Robbins
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 30
Get Book Here
Book Description
Author: William H. Robbins
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 30
Get Book Here
Book Description
Author: William H. Robbins
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 368
Get Book Here
Book Description
Author: John R. Howell
Publisher:
ISBN:
Category : Energy transfer
Languages : en
Pages : 44
Get Book Here
Book Description
An analytical technique suitable for & the solution of complex energy transfer problems involving coupled radiant and convective energy transfer is developed. Solutions for the coupled axial wall energy flax distribution in rocket nozzles using hydrogen as a propellant are presented. Flow rates and temperatures studied are near those forecast for gaseous-core nuclear-propulsion systems. Parameters varied are nozzle shape, inlet propellant temperature, mean reactor cavity temperature, and nozzle wall temperature level. The effects of variation of the propellant radiation absorption coefficient with pressure, temperature, and wavelength are presented, and real property variations are used where they appear to be significant. Comparison is made to a simplified, coupled solution using a modified second-order one-dimensional diffusion equation for the radiative transfer. At the temperature levels assumed, radiative transfer may account for a greater portion of the total energy transfer over important portions of the nozzle, and its effects cannot, therefore, be neglected. Extreme energy flaxes (near 3XlO to the 8 Btu/(hr)(sq ft)) are observed for certain cases, and this implies that new nozzle cooling techniques must be developed.
Author:
Publisher:
ISBN:
Category : Outer space
Languages : en
Pages : 544
Get Book Here
Book Description
A Chinese boy's greatest wish is to be an artist but he is too poor to buy a good brush until a wizard appears and gives him one with magic powers.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 498
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Astrophysics
Languages : en
Pages : 544
Get Book Here
Book Description
Author: Corrado Casci
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 416
Get Book Here
Book Description
