Transonic flow in ducts and nozzles; a survey

Hall, I.; Sutton, E. P.

doi:10.1007/978-3-642-88337-8_21

Cited by 6 publications

(3 citation statements)

References 24 publications

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“…An excellent survey of the early development of such methods can be found in Hall and Sutton. 48 The early methods including the more recent work of Martensen 49 and Martensen and von Sengbush 50 are primarily of historical interest because of the difficulty of evaluating coefficients of the double power series used in these solutions.…”

Section: Series Expansion Methodsmentioning

confidence: 99%

Survey of Methods for Exhaust-Nozzle Flow Analysis

Brown

Hamilton²

1976

Journal of Aircraft

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Section: Series Expansion Methodsmentioning

confidence: 99%

Survey of Methods for Exhaust-Nozzle Flow Analysis

Brown

Hamilton²

1976

Journal of Aircraft

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“…Sutton, of throat design published in Ref. 116. Later this work was extended (117) and a further paper included the effect of a centre body at the throat (118) whilst the original method was used as the starting point for the design of Mach 3 liners for the supersonic tunnel (119) .…”

Section: The Department Of the Mechanics Of Fluids And Its Successorsmentioning

confidence: 99%

The Victoria University of Manchester’s contributions to the development of aeronautics

Ackroyd

2007

Aeronaut. j.

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This issue of the Aeronautical Journal celebrates the 50th anniversary of the foundation of the Honours Degree Course in Aeronautical Engineering at the Victoria University of Manchester. The following article therefore describes the aeronautical research and teaching activities of that university up to its recent amalgamation with the University of Manchester Institute of Science and Technology (UMIST) to form the present-day University of Manchester. This juncture provides a further justification for recording the Victoria University’s achievements.Both the Victoria University and UMIST had their roots in the nineteenth century although, apart from the relatively brief period of the First World War, neither of them was particularly involved in aeronautics until after the Second World War. However, as Sections 6.0-10.0 seek to demonstrate, thereafter the Victoria University’s involvement became considerable. The preceding Sections describe the origins of the Victoria University and UMIST and, in the case of the former institution, the subsequent activities of its staff and graduates in engineering and mathematics which, although not always specifically aeronautical in content, nonetheless had a profound influence on the development of the aeronautical sciences.

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“…From one-dimensional considerations, it is well known [13] that the Iacceleration at the throat of a supersonic nozzle is given by Also from the dominant terms in boundary conditions (111-18) and (111-19), it is known that…”

Section: 1mentioning

confidence: 99%

A Theoretical and Experimental Investigation of Transonic Flow in the Throat Region of Annular Axisymmetric, Supersonic Nozzles.

Dutton¹,

Addy²

1980

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Transonic Flow Annular Nozzle Supersonic NozzleAn integrated theoretical and experimental investigation of flow in the throat region of unconventional, annular, supersonic nozzles was conducted. The theoretical analysis consists of the formulation and development of an approximate series expansion solution to the inviscid, irrotational governing equations. The resulting solution provides a direct means of analyzing the throat flowfields in a variety of two-dimensional nozzle configurations includ- Flowfield static pressure measurements were obtained for four nozzle configurations including an axisymmetric, Laval nozzle and three annular ones. Half-section cylindrical models were constructed and mounted on a splitter plate whose surface corresponds to a plane of symmetry for the axisymmetric geometries under consideration. Readings from a grid of pressure taps arranged on the splitter plate allowed the determination of the static pressure fields in the nozzle throats. For all four cases tested, it was found that the agreement between the theoretical and experimental results is quite good through a significant region of the throat. Only near the bounding walls in the throat inlet region was there a noticeable discrepancy for some of the cases.

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Transonic flow in ducts and nozzles; a survey

Cited by 6 publications

References 24 publications

Survey of Methods for Exhaust-Nozzle Flow Analysis

Survey of Methods for Exhaust-Nozzle Flow Analysis

The Victoria University of Manchester’s contributions to the development of aeronautics

A Theoretical and Experimental Investigation of Transonic Flow in the Throat Region of Annular Axisymmetric, Supersonic Nozzles.

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