DMCA

Results of Aerothermodynamic and Boundary Layer Transition Testing of 0.0362-Scale X-38 (Rev 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel (1997)

by Nasa Langley -inch Mach Tunnel , Scott A. Berry , Scott A. Berry , Thomas J. Horvath , Jr. , Thomas J. Horvath , V. Eric Roback , V. Eric Roback , George B. Williams , George B. Williams
Citations:2 - 1 self