Author : Richard I. Gomberg
Publisher :
Page : 44 pages
File Size : 21,10 MB
Release : 1978
Category :
ISBN :
[PDF] Effects Of Entrained Water And Strong Turbulence On Afterburning Within Solid Rocket Motor Plumes eBook
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Effects of Entrained Water and Strong Turbulence on Afterburining Within Solid Rocket Motor Plumes
Author : Richard I. Gomberg
Publisher :
Page : 42 pages
File Size : 19,10 MB
Release : 1978
Category : Aircraft exhaust emissions
ISBN :
NASA Technical Paper
Author :
Publisher :
Page : 192 pages
File Size : 48,64 MB
Release : 1983
Category : Astronautics
ISBN :
Scientific and Technical Aerospace Reports
Author :
Publisher :
Page : 1018 pages
File Size : 33,4 MB
Release : 1978
Category : Aeronautics
ISBN :
A computer simulation of the afterburning processes occurring within solid rocket motor plumes in the troposphere
Author : Richard I. Gomberg
Publisher :
Page : 52 pages
File Size : 12,85 MB
Release : 1976
Category : Solid propellant rockets
ISBN :
NASA Scientific and Technical Publications
Author :
Publisher :
Page : 410 pages
File Size : 43,9 MB
Release : 1987
Category : Aeronautics
ISBN :
Monthly Catalogue, United States Public Documents
Author :
Publisher :
Page : 546 pages
File Size : 34,88 MB
Release : 1978
Category : Government publications
ISBN :
Combined Experimental-analytical Investigation of Afterburning Solid Rocket Exhaust Plume Properties to Improve Signature Level Prediction Capability
Author :
Publisher :
Page : 190 pages
File Size : 27,7 MB
Release : 1990
Category :
ISBN :
Describes experimental work performed on a high-speed pre-mixed hydrogen-air jet flame in a co-flowing annular air flow in the presence and absence of base flow at the exit. Includes details on the high-speed flame in a coaxial air facility which was designed, built, and tested to simulate (in a first approximation) rocket exhaust flow conditions. In addition, a new high spatial resolution computer-controlled three-dimensional gear was built to traverse the investigated flow field. The main experimental tool was a two-dimensional laser Doppler velocimeter with data acquisition and processing system. The tool was used to measure the two main velocity components. Other measurements included turbulence intensities and mean temperatures at various downstream sections. The measured initial and flow field data will serve to evaluate the validity of various turbulence models and to predict the structure of rocket exhaust plumes. Moreover, the experiments established the effect of the base flow on the turbulence structure of the exhaust plume.
Government Reports Annual Index
Author :
Publisher :
Page : 1064 pages
File Size : 11,58 MB
Release : 1978
Category : Government reports announcements & index
ISBN :
Rocket Exhaust Ground Cloud/atmospheric Interactions
Author : BaoChuan Hwang
Publisher :
Page : 196 pages
File Size : 38,4 MB
Release : 1978
Category : Air
ISBN :