An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 /

Bibliographic Details

Main Author:	Prabhu, Ramadas K.
Corporate Author:	Langley Research Center
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information, [2001]
Series:	NASA contractor report ; NASA CR-211266.
Subjects:	Aerodynamic characteristics. Aeroshells. COMPUTATIONAL FLUID DYNAMICS. Inviscid flow. Mach number. Mars missions. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS39078