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FIXED-BASE SIMULATOR STUDY OF AN EXTERNALLY BLOWN FLAP STOL TRANSPORT AIRPLANE DURING APPROACH AND LANDING

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BookPublisher: Nasa, Washington, D.C. 1972Description: 97.DDC classification: NASA | TN D-6898

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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	NASA TN D-6898 (Browse shelf)	Not for loan		TR12799

Total holds: 0

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Previous	NASA TN D-6895 NUMERICAL ANALYSIS OF THE TRANSIENT RESPONSE OF AN AXISYMMETRIC ABLATIVE CHAR LAYER CONSIDERING INTERNAL FLOW EFFECTS	NASA TN D-6896 THE EFFECTS OF CONFIGURATION CHANGES ON THE AERODYNAMIC CHARACTERISTICS OF A FULL-SCALE MOCKUP OF A LIGHT TWIN-ENGINE AIRPLANE	NASA TN D-6897 EFFECT OF JET CONVERGENCE ANGLE ON THE PERFORMANCE OF ANNULAR NOZZLES WITH SEMITOROIDAL CONCAVE PLUGS AT A MACH NUMBERS UP TO 1.82	NASA TN D-6898 FIXED-BASE SIMULATOR STUDY OF AN EXTERNALLY BLOWN FLAP STOL TRANSPORT AIRPLANE DURING APPROACH AND LANDING	NASA TN D-6899 FATIGUE CRACK GROWTH FROM A CIRCULAR HOLE WITH AND WITHOUT HIGH PRIOR LOADING	NASA TN D-6911 STRUCTURE OF ZIRCONIUM-93 AND ZIRCONIUM-91 AS SHOWN BY THE REACTIONS 92ZR(D,P) 93ZR AND 92ZR(D,T)91ZR	NASA TN D-6912 INFLUENCE OF ALLOYING ELEMENTS ON FRICTION AND WEAR OF COPPER	Next

Bound With Nasa Tn D-6890-97, 6899

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