Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊

A wind-tunnel investigation of sonic-boom pressure distributions of bodies of revolution at Mach 2.96, 3.83, and 4.63

Barrett L. Shrout

Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds

William A. Cassels

Flexion des coques de révolution soumises à des champs axisymétriques de forces et de températures

Severin Casacci

Studies of the turbulent boundary layer on a waisted body of revolution in subsonic and supersonic flow

Kenneth George Winter

Sverkhzvukovoe obtekanie tel neodnorodnym potokom idealʹnogo gaza

V. F. Kamenet͡skiĭ

The incompressible laminar boundary layer over a slender body of revolution at small incidence

T. R. F. Nonweiler