Piezoelectric polymer transducers for dynamic pressure measurements. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.

Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3

Instrumentation for force and pressure measurements in a hypersonic shock tunnel

Mode of access: Internet.