EXPERIMENTAL AND THEORITICAL ANALYSIS OF ABLATIVE MATERIAL RESPONSE IN A LIQUID PROPELLANT ROCKET ENGINE
Material type:
- 629.134354 EX71
Item type | Current library | Collection | Call number | URL | Status | Date due | Barcode | Item holds | |
---|---|---|---|---|---|---|---|---|---|
![]() |
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | 629.134354 EX71 (Browse shelf(Opens below)) | Link to resource | Available | A77718 |
Total holds: 0
Browsing PK Kelkar Library, IIT Kanpur shelves, Collection: COMPACT STORAGE (BASEMENT) Close shelf browser (Hides shelf browser)
![]() |
![]() |
No cover image available | No cover image available | No cover image available | No cover image available | No cover image available | ||
629.1343535 H999 HYPERSONIC AIRBREATHING PROPULSION | 629.1343537 R418a Advanced control of turbofan engines | 629.134354 Am35 Sounding rocket: Collection of technical papers | 629.134354 EX71 EXPERIMENTAL AND THEORITICAL ANALYSIS OF ABLATIVE MATERIAL RESPONSE IN A LIQUID PROPELLANT ROCKET ENGINE | 629.134354 N811a ADVANCES IN TACTICAL ROCKET PROPULSION | 629.134354 T343 THEORY AND ANALYSIS OF A HIGHLY ELASTIC LAUNEH VEHICHLE | 629.13436 C175f Finite difference modeling of rotor flows including wake effects |
There are no comments on this title.
Log in to your account to post a comment.