EFFECT OF TIP VORTEX STRUCTURE OF HELICOPTER NOISE DUE TO BLADE
Material type:
TextSeries: Nasa-Cr-152150, M. I. T. Fluid Dynamics Research Laboratory Report ; 78-2Publication details: Massachusetts Institute Of Technology 1978Description: 94Subject(s): DDC classification: - 629.1323 W831e
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|
| Written-off | PK Kelkar Library, IIT Kanpur | Written-of | 629.1323 W831e (Browse shelf(Opens below)) | Not for loan | A77730 |
Total holds: 0
Browsing PK Kelkar Library, IIT Kanpur shelves 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 | ||
| 629.1323 SCH39AE AERODYNAMICS OF THE AIRPLANE | 629.1323 St84b BASIC AERODYNAMICS | 629.1323 St84b BASIC AERODYNAMICS | 629.1323 W831e EFFECT OF TIP VORTEX STRUCTURE OF HELICOPTER NOISE DUE TO BLADE | 629.13230151 AM35C A COLLECTION OF TECHNICAL PAPERS | 629.13232 B729t TURBULENCE MEASUREMENTS WITH HOT WIRE ANEMOMETERS | 629.13232 Sch39c CALCULATION OF THE FRICTIONLESS INCOMPRESSIBLE FLOW FOR A GIVEN TWO-DIMENSIONAL CASCADE |
There are no comments on this title.
Log in to your account to post a comment.