Summary goes here
সংরক্ষণ করুন:
| বিন্যাস: | গ্রন্থ |
|---|---|
| ভাষা: | ইংরেজি |
| বিষয়গুলি: | |
| ট্যাগগুলো: |
ট্যাগ যুক্ত করুন
কোনো ট্যাগ নেই, প্রথমজন হিসাবে ট্যাগ করুন!
|
| era | |
|---|---|
| format | Book |
| genre | |
| geographic | |
| id | 00319c4e-0fda-438a-985f-62d171d4cbd6 |
| isbn | |
| issn | |
| language | eng |
| physical | 1 volume. |
| publication | – publisher: National Aeronautics and Science Administration Langley Research Center dateOfPublication: 2001 |
| publishDate | 2001 |
| subjects | |
| title | Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees / Ramadas K. Prabhu. |
| topic | Aerodynamic characteristics. Aerodynamic coefficients. Angle of attack. Computational fluid dynamics. Hypersonic speed. Inviscid flow. Mach number. Space Shuttle orbiters. Electronic government information Government publications |