The Problem: Instantaneously Effecting Controlled Balloon-system Descent from High Altitude PDF Download
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Author: James F. Dwyer
Publisher:
ISBN:
Category : Balloons
Languages : en
Pages : 44
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Book Description
The need for a technique of instantaneously effect controlled balloon-system descent from high altitude prompted the development efforts reported herein. The background, the approach, test flight data, and the technical problems that frustrated the successful development of the desired technique are included. A simplified model of the shape of a partially full balloon is presented (a model that should also approximate the dimensions of subpressure shapes). Some heretofore unpublished information on apex valve characteristics and subpressure effects are included together with recommendations for any future work of this problem. Significant supplementary findings and historical perspectives are noted. (Author).
Author: James F. Dwyer
Publisher:
ISBN:
Category : Balloons
Languages : en
Pages : 44
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Book Description
The need for a technique of instantaneously effect controlled balloon-system descent from high altitude prompted the development efforts reported herein. The background, the approach, test flight data, and the technical problems that frustrated the successful development of the desired technique are included. A simplified model of the shape of a partially full balloon is presented (a model that should also approximate the dimensions of subpressure shapes). Some heretofore unpublished information on apex valve characteristics and subpressure effects are included together with recommendations for any future work of this problem. Significant supplementary findings and historical perspectives are noted. (Author).
Author: James F. Dwyer
Publisher:
ISBN:
Category : Balloon ascensions
Languages : en
Pages : 108
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Book Description
This paper critiques existing aerodynamic-thermodynamic models for predicting the vertical motion of free balloon systems. It demonstrates that: a) the aerodynamic drag coefficient model should be based on Froude number and fractional volume as well as Reynolds number; b) there has been a widespread error in definition of the instantaneous mass of the balloon film involved in the heat transfer process; c) the gas bubble cannot be modelled as a sphere; d) the gas bubble is asymmetrical except when near or at its natural ceiling altitude; and e) the actual gas bubble shape, and most probably the added mass, is directly related to the type of gore pattern. Finally, a procedure is proposed for the analysis of actual flight data to enable the development of a practical, but also theoretically sound, model of the aerodynamic drag coefficient of a zero-pressure, free balloon- and subsequent refinement of the heat transfer models for direct and reflected solar energy.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 788
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 172
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Book Description
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 948
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautical instruments
Languages : en
Pages : 230
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Book Description
Author: Technology Reports Centre (Great Britain)
Publisher:
ISBN:
Category :
Languages : en
Pages : 622
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Book Description
Author: W. Riedler
Publisher:
ISBN:
Category : Balloons
Languages : en
Pages : 156
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Book Description
Author: Y. Malméjac
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 810
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Book Description
Author: E. G. Ewing
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 502
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Book Description
This document serves as the third revision of the USAF Parachute Handbook which was first published in 1951. The data and information represent the current state of the art relative to recovery system design and development. The initial chapters describe representative recovery applications, components, subsystems, material, manufacture and testing. The final chapters provide empirical data and analytical methods useful for predicting performance and presenting a definitive design of selected components into a reliable recovery system.
