1-4 of 4 Books
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
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 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
Superalloy foams for aeroshell applications
Superalloy foams for aeroshell applications
By John Gayuda