Accession Number : AD0457270


Title :   CALCULATIONS FOR THE DESIGN OF NOZZLES.


Descriptive Note : Technical rept.,


Corporate Author : ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)


Personal Author(s) : Dodd, K N ; Piggott, B A M ; Day, B P


Report Date : Oct 1964


Pagination or Media Count : 14


Abstract : Details are given of the numerical procedures required in the design of an axially-symmetric nozzle. A velocity distribution along the axis of symmetry is assumed to be given and from this, a characteristic network is used to determine the isentropic core boundary after which a boundary layer calculation gives the shape of the nozzle itself. (Author)


Descriptors :   *ROCKET NOZZLES , AEROSPACE CRAFT , AXISYMMETRIC FLOW , ATTITUDE CONTROL SYSTEMS , BOUNDARY LAYER , CONFIGURATIONS


Distribution Statement : APPROVED FOR PUBLIC RELEASE