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Analysis Of A Jet In A Subsonic Crosswind

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Analysis Of A Jet In A Subsonic Crosswind

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Author :
language : en
Publisher:
Release Date : 1969

Analysis Of A Jet In A Subsonic Crosswind written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamics categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1979

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.

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.

Nasa Technical Report

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1973

Nasa Technical Report written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aerodynamics categories.

Analysis Of A Jet In A Subsonic Crosswind Nasa Symposium

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Author :
language : en
Publisher:
Release Date :

Analysis Of A Jet In A Subsonic Crosswind Nasa Symposium written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with categories.

A Method For Assessing The Impact Of Wake Vortices Of Usaf Operations

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Author : George Kurylowich
language : en
Publisher:
Release Date : 1979

A Method For Assessing The Impact Of Wake Vortices Of Usaf Operations written by George Kurylowich and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Helicopters categories.

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.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1975

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.

Analysis Of The Injection Of A Heated Turbulent Jet Into A Cross Flow

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Author : James Franklin Campbell
language : en
Publisher:
Release Date : 1973

Analysis Of The Injection Of A Heated Turbulent Jet Into A Cross Flow written by James Franklin Campbell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Jets categories.

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.