IHS ESDU Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds. 79004

Description
ESDU 79004 gives charts of forebody volume coefficient (ratio of forebody volume to that of the enclosing cylinder) and of wave drag for spherically blunted tangent ogives and paraboloids and modified ellipsoids in the Mach number range 0.7 to 1.05. The drag was obtained by integrating the surface pressure distribution, derived from a finite difference program for calculating inviscid transonic flow, to give a pressure drag that is assumed for these bodies at zero incidence to equal the wave drag. Computed pressure distribution data for a fineness ratio 2 forebody are compared with wind-tunnel measurements and found to agree closely.
Description
ESDU 79004 gives charts of forebody volume coefficient (ratio of forebody volume to that of the enclosing cylinder) and of wave drag for spherically blunted tangent ogives and paraboloids and modified ellipsoids in the Mach number range 0.7 to 1.05. The drag was obtained by integrating the surface pressure distribution, derived from a finite difference program for calculating inviscid transonic flow, to give a pressure drag that is assumed for these bodies at zero incidence to equal the wave drag. Computed pressure distribution data for a fineness ratio 2 forebody are compared with wind-tunnel measurements and found to agree closely.

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Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds. - 79004 - IHS ESDU
London, United Kingdom
Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds.
79004
Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds. 79004
ESDU 79004 gives charts of forebody volume coefficient (ratio of forebody volume to that of the enclosing cylinder) and of wave drag for spherically blunted tangent ogives and paraboloids and modified ellipsoids in the Mach number range 0.7 to 1.05. The drag was obtained by integrating the surface pressure distribution, derived from a finite difference program for calculating inviscid transonic flow, to give a pressure drag that is assumed for these bodies at zero incidence to equal the wave drag. Computed pressure distribution data for a fineness ratio 2 forebody are compared with wind-tunnel measurements and found to agree closely.

ESDU 79004 gives charts of forebody volume coefficient (ratio of forebody volume to that of the enclosing cylinder) and of wave drag for spherically blunted tangent ogives and paraboloids and modified ellipsoids in the Mach number range 0.7 to 1.05. The drag was obtained by integrating the surface pressure distribution, derived from a finite difference program for calculating inviscid transonic flow, to give a pressure drag that is assumed for these bodies at zero incidence to equal the wave drag. Computed pressure distribution data for a fineness ratio 2 forebody are compared with wind-tunnel measurements and found to agree closely.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 79004
Product Name Forebodies of fineness ratio 1.0, 1.5 and 2.0, having low values of wave drag coefficient at transonic speeds.
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