Normal view MARC view ISBD view

STABILITY INVESTIGATION OF A BLUNTED CONE AND A BLUNTED OGIVE WITH A FLARED CYLINDER AFTERBODY AT MACH NUMBERS FROM 0.30 TO 2.85

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1962Description: 27.DDC classification: NASA | TN D-1506

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1506 (Browse shelf)	Not for loan		TR11470

Total holds: 0

Previous								Next
Previous	NASA TN D-1503 HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON A HEMISPHERE-CYLINDER AND A BLUFF-AFTERBODY MODEL IN METHANE-AIR COMBUSTION PRODUCTS AND IN AIR	NASA TN D-1504 A REPORT ON THE RESEARCH AND TECHNOLOGICAL PROBLEMS OF MANNED ROTATING SPACECRAFT	NASA TN D-1505 THE BENDING-MOMENT DISTRIBUTION OF CAMBERED-SPAN WING SYSTEMS HAVING MINIMUM INDUCED DRAG	NASA TN D-1506 STABILITY INVESTIGATION OF A BLUNTED CONE AND A BLUNTED OGIVE WITH A FLARED CYLINDER AFTERBODY AT MACH NUMBERS FROM 0.30 TO 2.85	NASA TN D-1507 PRESSURE DISTRIBUTION INDUCED ON A FLAT PLATE AT A FREE-STREAM MACH NUMBER OF 1.39 BY ROCKETS EXHAUSTING UPSTREAM AND DOWNSTREAM	NASA TN D-1508 STATIC STABILITY TESTS IN THE LANGLEY 24-INCH HYPERSONIC ARC TUNNEL ON A BLUNTED CONE AT MACH NUMBER OF 20	NASA TN D-1509 PROPELLER SLIPSTREAM EFFECTS AS DETERMINED FROM WING PRESSURE DISTRIBUTION ON A LARGE-SCALE SIX-PROPELLER VTOL MODEL AT STATIC THRUST	Next

Bound With Nasa Tn D-1501-1505, 1507-1509.

There are no comments for this item.

PKK Library