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SHOCK CAPTURING METHOD FOR CALCULATING SUPERSONIC FLOW FIELDS

By: Walken,F.

Contributor(s): Caine,P.

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BookSeries: Aeronautical Research Council Current Papers Cp-1290. Publisher: Her Majestys Stationery Office, London 1974Description: 29.DDC classification: TR | CP-1290

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	TR CP-1290 (Browse shelf)	Not for loan Untraceable		TR3307

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

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Previous	TR CP-1287 CIVIL AIRCRAFT AIRWORTHINESS DATA RECORDING PROGRAMME UNEVEN RUNWAYS ENCOUNTERED BY SUBSONIC JET TRANSPORT AIRCRAFT DURING SCHEDULED AIRLINE OPERATIONS	TR CP-1288 AEROELASTIC MODEL HELICOPTER ROTOR	TR CP-1289 STUDY OF SOLID STATE REMOTE CONTROL TECHNIQUES AS APPLIED TO THE REDESIGN OF THE ELECTRICAL SYSTEM IN A LARGE CIVIL AIRCRAFT	TR CP-1290 SHOCK CAPTURING METHOD FOR CALCULATING SUPERSONIC FLOW FIELDS	TR CP-1291 MEASUREMENT OF THE ITERNAL PERFORMANCE OF A RECTANGULAR AIR INTAKE MOUNTED ON A FUSELAGE AT MACH NUMBERS FROM 1.6 TO 2	TR CP-1293 LOW-SPEED WIND-TUNNEL TESTS ON THE LIFT-DEPENDENT DRAG OF DELTA WINGS WITH CONICAL CAMBER	TR CP-1297 VARIABILITY OF FATIGUE DAMAGE FROM FLIGHT TO FLIGHT	Next

Bound With: Arc Cp No. 1281-1290

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