In conjunction with an earlier transonic test, a 0.04-scale model of the Saturn V launch vehicle was tested at Mach numbers from 1.80 to 3.00 for Reynolds number based on model diameter varying from 1.59 to 2.77 million. Static pressure distributions and boundary-layer profiles were measured and are presented herein.
Pressure Test on a 0.04-Scale Model of the Saturn V Launch Vehicle at Mach Numbers from 1.80 Through 3.00
1967
43 pages
Report
No indication
English