Free-flight tests to determine the power-on and power-off pressure distribution and drag of the NACA RM-10 research vehicle at large Reynolds numbers between Mach numbers 0.8 and 3.0

Hoffman, Sherwood
naca-rm-l55h02
September 20, 1955


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-l55h02.pdf