ESDU 80021:1989

$62.40

Pressure drag of blunt forebodies at zero incidence for Mach numbers up to 10

Published By	Publication Date	Number of Pages
ESDU	1989-04-01	20

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ESDU 80021 provides data for the pressure drag component of the forebody drag for families of ellipsoidal, tangent ogive, spherically-blunted tangent ogive and flat-faced forebodies with and without a radiused shoulder. The bodies are at zero incidence and at subsonic, supersonic and hypersonic speeds up to Mach 10 except for the tangent ogive for which the data apply up to a Mach number of 4.5. The information is presented in graphical form, and was obtained from correlations of experimental data and theoretical calculations for inviscid airflow.


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Published Code	ESDU
Published By	ESDU
Publication Date	1989-04-01
Pages Count	20
Language	English
File Size	512.0 KB

ESDU 80021:1989

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