Normal view MARC view ISBD view

THEORETICAL PRESSURE DISTRIBUTIONS ON WINGS OF FINITE SPAN AT ZERO INCIDENCE FOR MACH NUMBERS NEAR 1

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1961Description: 47.DDC classification: NASA | TR R-88

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 TR R-88 (Browse shelf)	Not for loan		TR14361

Total holds: 0

Previous								Next
Previous	NASA TR R-85 A NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON	NASA TR R-86 THE DRAG COEFFICIENT OF PARABOLIC BODIES OF REVOLUTION OPERATING AT ZERO CAVITATION NUMBER AND ZERO ANGLE OF YAW	NASA TR R-87 A STUDY OF THE POSITIONS AND VELOSCITIES OF A SPACE STATION AND A FERRY VEHICLE DURING RENDEZVOUS AND RETURN	NASA TR R-88 THEORETICAL PRESSURE DISTRIBUTIONS ON WINGS OF FINITE SPAN AT ZERO INCIDENCE FOR MACH NUMBERS NEAR 1	NASA TR R-89 TRAJECTORY CONTROL FOR VEHICLES ENTERING THE EARTH`S ATMOSPHERE AT SMALL FLIGHT-PATH ANGLES	NASA TR R-90 THEORY AND APPARATUS FOR MEASUREMENT OF EMISSIVITY FOR RADIATIVE COOLING OF HYPERSONIC AIRCRAFT WITH DATA FOR INCONEL, INCONEL X, STAINLESS STEEL 303, AND TITANIUM ALLOY RS-120	NASA TR R-92 AN INVESTIGATION OF THE EFFECT OF HIGH TEMPERATURE OF THE SCHUMANN-RUNGE ULTRAVIOLET ABSORPTION CONTINUUM OF OXYGEN	Next

Bound With Nasa Tr R-81-87,89-90

There are no comments for this item.

PKK Library