SUPERSONIC FLOW AND SHOCK WAVES
Material type:
- 629.51 C825s
Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
---|---|---|---|---|---|---|---|---|
![]() |
PK Kelkar Library, IIT Kanpur | General Stacks | 629.51 C825s (Browse shelf(Opens below)) | Available | A71614 |
Browsing PK Kelkar Library, IIT Kanpur shelves, Collection: General Stacks 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 | No cover image available | No cover image available | ||
629.51 B31t Theory of homogeneous turbulence | 629.51 B54a AEROELASTICITY | 629.51 C17aE HIGH-SPEED AERODYNAMICS | 629.51 C825s SUPERSONIC FLOW AND SHOCK WAVES | 629.51 C825s Supersonic flow and shock waves | 629.51 D713a AERODYNAMICS COMPONENTS OF AIRCRAFT AT HIGH SPEEDS | 629.51 D885s6 SOUND BARRIER |
Receding Shock Wave (Illus.) : Leaf Inserted
Originates From A Report Issued In 1944 Under The Auspices Of The Office Of Scientific Research Development
Also Published As Applied Mathematical Science ; V. 2 By Springer Verlag
There are no comments on this title.