Effect of Geometric Parameters on the Static Performance of an Annular Nozzle with a Concave Central Base PDF Download
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Author: Charles E. Mercer
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
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Book Description
Author: Charles E. Mercer
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 798
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 720
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
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Book Description
Author: Charles E. Mercer (Aerospace engineer)
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 40
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Book Description
Author: Charles E. Mercer
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 116
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Book Description
Results of an investigation at static conditions and at Mach numbers up to 1.82 are presented for 12 nozzle configurations which have jet convergence angle and jet throat area as geometric parameters. The variation of jet convergence angle from 15 to 40 deg had little effect on the performance of the nozzles having the large value of primary throat area; however, increasing jet convergence angle generally had an adverse effect on performance of the nozzles having the smaller value of primary throat area. The performance of the nozzle configurations with the larger primary throat area is competitive with nozzles designed for operation over the Mach number range.
Author: Blake W. Jr Corson
Publisher:
ISBN:
Category :
Languages : en
Pages : 70
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Author: Blake W. Corson (Jr)
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 22
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Book Description
A static test of an annular nozzle with a concave central base, producing a jet in which tangents to the jet streamlines at the exit converged toward a region on the axis of symmetry downstream of the exit, has indicated good thrust performance. A value of nozzle-flow coefficient only slightly less than unity indicates the internal loss to be small. Pressures on the concave central base are relatively large and positive, and a predictable portion of the total thrust of the jet is exerted on the central base.
Author: William B. Compton
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 60
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Author: University of Toronto. Institute for Aerospace Studies
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 764
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