1-4 of 4 Books
An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By Ramadas K. Prabhu
Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
By Ramadas K. Prabhu
Superalloy foams for aeroshell applications
Superalloy foams for aeroshell applications
By John Gayuda
Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
By Ramadas K. Prabhu