Analysis of a Jet in a Subsonic Crosswind
Author :
Publisher :
Page : 260 pages
File Size : 22,34 MB
Release : 1969
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 260 pages
File Size : 22,34 MB
Release : 1969
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 249 pages
File Size : 35,99 MB
Release : 1969
Category :
ISBN :
Author :
Publisher :
Page : pages
File Size : 19,40 MB
Release :
Category :
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 249 pages
File Size : 23,76 MB
Release : 1969
Category :
ISBN :
Author : National Aeronautics and Space Administration, Scientific and Technical Information Division
Publisher :
Page : pages
File Size : 47,23 MB
Release : 1969
Category :
ISBN :
Author :
Publisher :
Page : 662 pages
File Size : 27,22 MB
Release : 1982
Category : Aeronautics
ISBN :
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.
Author : James Franklin Campbell
Publisher :
Page : 70 pages
File Size : 35,89 MB
Release : 1973
Category : Jets
ISBN :
An investigation has been undertaken to develop a theoretical model of the incompressible jet injection process. The discharge of a turbulent jet into a cross flow was mathematically modeled by using an integral method which accounts for natural fluid mechanisms such as turbulence, entrainment, buoyancy, and heat transfer. The analytical results are supported by experimental data and demonstrate the usefulness of the theory for estimating the trajectory and flow properties of the jet for a variety of injection conditions. The capability of predicting jet flow properties, as well as two- and three- dimensional jet paths, was enhanced by obtaining the jet cross-sectional area during the solution of the conservation equations (a number of previous studies assume a specific growth for the area). Realistic estimates of temperature in the jet fluid were acquired by accounting for heat losses in the jet flow due to forced convection and to entrainment of free-stream fluid into the jet.
Author :
Publisher :
Page : 758 pages
File Size : 50,33 MB
Release : 1970
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 606 pages
File Size : 10,73 MB
Release : 1975
Category :
ISBN :
Author :
Publisher :
Page : 776 pages
File Size : 34,58 MB
Release : 1971
Category : Mechanics, Applied
ISBN :