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HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS INSIDE THE HINGE-LINE GAP OF A WEDGE-FLAP COMBINATION AT MACH NUMBER 10.4

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BookPublisher: NASA, WASHINGTON, D.C. 1968Description: ,55.DDC classification: NASA | TN D-4911

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-4911 (Browse shelf)	Not for loan		101122

Total holds: 0

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Previous	NASA TN D-4841 USE OF AN ELECTROLUMINESCENT DISPLAY IN MANUAL TRACKING AND IN A READING TASK.	NASA TN D-4861 COMPARISON OF INFORMATION DISPLAY CONCEPTS FOR LANDING OF VTOL AIRCRAFT	NASA TN D-4881 EFFECTS OF TURBULENT MIXING ON AVARAGE FUEL TEMPERATURES IN A GAS-CORE NUCLEAR ROCKET ENGINE.	NASA TN D-4911 HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS INSIDE THE HINGE-LINE GAP OF A WEDGE-FLAP COMBINATION AT MACH NUMBER 10.4	NASA TN D-4921 BUCKLING OF AN EQUATORIAL SEGMENT OF A SPHERICAL SHELL LOADED BY ITS OWN WEIGHT	NASA TN D-4931 FLYING QUALITY FACTORS CURRENTLY LIMITING HELICOPTER NAP-OF-THE-EARTH MANEUVERABILITY AS INDENTIFIED BY FLIGHT INVESTIGATION	NASA TN D-4961 EFFECT OF UNIT REYNOLDS NUMBER, NOSE BLUNTESS, ANGLE OF ATTACK, AND ROUGHNESS ON TRANSITION ON A 5 (DEGRE) HALF-ANGLE CONE AT MACH 8	Next

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