Book Description
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 :
Publisher :
Page : 662 pages
File Size : 10,79 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 :
Publisher :
Page : 758 pages
File Size : 48,69 MB
Release : 1970
Category : Aerodynamics
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Author : George Kurylowich
Publisher :
Page : 114 pages
File Size : 24,56 MB
Release : 1979
Category : Helicopters
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Experience as a consultant to the Safety Office at Norton AFB led to compiling the engineering tools presented so that this report can be used by engineering personnel to investigate future incidents/accidents and existing USAF operations that are impacted by the vortical wake hazard. The approach presented is amenable to easy hand computations. Mixed airplane/helicopter operations can be assessed, since the engineering tools to determine the location and strength of the rotor downwash field behind a helicopter are presented. Finally, a simplified mathematical model is given to represent this hazard for use in USAF simulators, to make pilots aware of the problems associated with operating in wake-contaminated airspace.
Author : James Franklin Campbell
Publisher :
Page : 70 pages
File Size : 42,59 MB
Release : 1973
Category : Jets
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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 : United States. National Aeronautics and Space Administration
Publisher :
Page : 936 pages
File Size : 21,48 MB
Release : 1973
Category : Aerodynamics
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Author :
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Page : 606 pages
File Size : 24,39 MB
Release : 1975
Category :
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Author :
Publisher :
Page : 1250 pages
File Size : 27,29 MB
Release : 1970
Category : Government publications
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Author : United States. Superintendent of Documents
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Page : 1320 pages
File Size : 42,80 MB
Release : 1966
Category : Government publications
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Author : United States. Superintendent of Documents
Publisher :
Page : 1348 pages
File Size : 23,23 MB
Release : 1970
Category : United States
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Author : Wen-Jei Yang
Publisher : Springer
Page : 576 pages
File Size : 24,23 MB
Release : 1987
Category : Fluid dynamics
ISBN :