HYPERSONIC FACILITIES IN THE AERODYNAMICS DEPARTMENT ROYAL AIRCRAFT ESTABLISHMENT
By: Hufton,P A.
Material type:![materialTypeLabel](/opac-tmpl/lib/famfamfam/BK.png)
Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
![]() |
PK Kelkar Library, IIT Kanpur | General Stacks | NATO AGARD 146 (Browse shelf) | Not for loan | TR16773 |
Total holds: 0
Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser
NATO AGARD 143 TUBE WIND TUNNEL A SPECIAL TYPE OF BLOWDOWN TUNNEL | NATO AGARD 144 THE SHOCK TUNNEL AND ITS APPLICATIONS TO HYPERSONIC FLIGHT | NATO AGARD 145 PHYSICAL GAS DYNAMICS RESEARCH AT THE AVCO RESEARCH LABORATORY | NATO AGARD 146 HYPERSONIC FACILITIES IN THE AERODYNAMICS DEPARTMENT ROYAL AIRCRAFT ESTABLISHMENT | NATO AGARD 147 HYPERSONIC SHOCK TUBE EQUIPMENT AT THE NATIONAL PHYSICAL LABORATORY, U.K. | NATO AGARD 148 MEASUREMENT OF PILOT MENTAL EFFORT | NATO AGARD 149 STRUCTURES ET CHALEUR AUX VITESSES SUPERSONIQUES ET HYPERSONIQUES |
Bound With Nato Agard 141-145, 147-149
There are no comments for this item.