Aerodynamic facilitiesHypersonic shock tunnel and free piston shock tube studies of sixty degree half-angle cones to determine validity of theories of laminar convective heat transfer in planetary gases
IDRelationTitle19680027925Collected WorksSpace programs summary no. 37-51, volume 3 for the period April 1 to May 31, 1968. Supporting research and advanced developmentCollected Works19680027925Collected WorksSpace programs summary no. 37-51, volume 3 for the period April 1 to May 31, 1968. Supporting research and advanced developmentN68-37397 23-11Collected Works