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COMPARISON OF INFORMATION DISPLAY CONCEPTS FOR LANDING OF VTOL AIRCRAFT

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BookPublisher: NASA, WASHINGTON, D.C. 1968Description: ,42.DDC classification: NASA | TN D-4861

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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-4861 (Browse shelf)	Not for loan		101117

Total holds: 0

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Previous	NASA TN D-4804 Effects of reduced airspeed for landing approach on flying qualities of a large jet transport equipped with powered lift [NASA TN D-4804]	NASA TN D4811 SIMPLIFIED TECHNIQUE FOR DETERMINING PERICYNTHION ALTITUDE OF LUNAR ORBITS	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	Next

Bound with NASA TN D-4862-4870

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