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Author: Ralph Edward Phinney
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
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Book Description
An experimental study of the control forces and moments generated by a slot-type secondary jet located near the base of an ogive cylinder in a Mach 4 and 5 free stream was conducted in the NOL Supersonic Tunnel No. 2. The free-stream Reynolds number, based on body length, was held constant at 22,000,000 and the missile angle of attack was varied from -10 to +10 degrees. The jet slot spanned one quadrant of the cylindrical surface and was contained between two low aspect ratio fins. (Author).
![Slot Jet Interaction Studies of an Ogive Cylinder at M[infinity] PDF](https://books.google.com/books/content/images/frontcover/u_2ZjqmUfeUC?fife=w80-h100)
Author: Ralph Edward Phinney
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
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Book Description
An experimental study of the control forces and moments generated by a slot-type secondary jet located near the base of an ogive cylinder in a Mach 4 and 5 free stream was conducted in the NOL Supersonic Tunnel No. 2. The free-stream Reynolds number, based on body length, was held constant at 22,000,000 and the missile angle of attack was varied from -10 to +10 degrees. The jet slot spanned one quadrant of the cylindrical surface and was contained between two low aspect ratio fins. (Author).
Author: R. E. Phinney
Publisher:
ISBN:
Category :
Languages : en
Pages : 57
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Book Description
An experimental study of the control forces and moments generated by a slot-type secondary jet located near the base of an ogive cylinder in a Mach 4 and 5 free stream was conducted in the NOL Supersonic Tunnel No. 2. The free-stream Reynolds number, based on body length, was held constant at 22,000,000 and the missile angle of attack was varied from -10 to +10 degrees. The jet slot spanned one quadrant of the cylindrical surface and was contained between two low aspect ratio fins. (Author).
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 992
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Author: Louis A. Cassel
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 420
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Book Description
Interference effects between a highly underexpanded, sonic or supersonic jet in a subsonic or supersonic crossflow, and the surface from which the jet exhausts are examined. For subsonic freestream Mach numbers, existing data are examined and correlated. Various semi-empirical models to represent the interference pressure distribution on flat plates are then developed. For supersonic freestream Mach numbers, a computer program for calculating jet interference effects on axisymmetric bodies at angle of attack is described. Interference effects between the jet plume and control fins on a cruciform missile are analyzed. A semi-empirical model of the jet in a crossflow, valid at large distances from the nozzle is developed. The results of this model are then used to compute interference forces and moments on fins located aft of the nozzle, both for subsonic and for supersonic freestream Mach numbers.
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 810
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
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Author: International Council of the Aeronautical Sciences. Congress
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1174
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 376
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 992
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Book Description
