Accession Number : AD0782968

Title :   An Approximate Transonic Calculative Method Applied to Various Smooth Shaped Nose-Cylindrical Bodies.

Descriptive Note : Technical rept.,

Corporate Author : TENNESSEE UNIV SPACE INST TULLAHOMA

Personal Author(s) : Venghaus,Heinz H. ; Wu,Jain-Ming

Report Date : 10 MAY 1974

Pagination or Media Count : 33

Abstract : An approximate transonic small disturbance technique originally developed for ogival noses and cylindrical afterbodies has been extended to arbitrary smooth nose forebodies and cylindrical afterbodies. Limitations of the method and trends are discussed. (Author)

Descriptors :   *Projectiles, *Nose cones, Transonic flow, Cylindrical bodies, Ogives, Free stream, Flow fields, Approximation(Mathematics)

Subject Categories : Guided Missiles
      Ammunition and Explosives
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE