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APPLICATION OF THE LEADING-EDGE-SUCTION ANALOGY TO PREDICTION OF LONGITUDINAL LOAD DISTRIBUTION AND PITCHING MOMENTS FOR SHARP-EDGED DELTA WINGS

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BookPublisher: Nasa, Washington, D.C. 1972Description: 20.DDC classification: NASA | TN D-6994

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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-6994 (Browse shelf)	Not for loan		TR12378

Total holds: 0

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Previous	NASA TN D6991 CALIBRATION OF RADIATION DETECTORS IN THE ULTRAVIOLET REGION BETWEEN 972 AND 2500 A.	NASA TN D-6992 STUDY OF AIRCRAFT-CENTERED NAVIGATION, GUIDANCE, AND TRAFFIC SITUATION SYSTEM CONCEPT FOR TERMINAL-AREA OPERATION.	NASA TN D-6993 SUMMARY OF DIRECTIONAL DIVERGENCE CHARACTERISTICS OF SEVERAL HIGH-PERFORMANCE AIRCRAFT CONFIGURATIONS.	NASA TN D-6994 APPLICATION OF THE LEADING-EDGE-SUCTION ANALOGY TO PREDICTION OF LONGITUDINAL LOAD DISTRIBUTION AND PITCHING MOMENTS FOR SHARP-EDGED DELTA WINGS	NASA TN D-6995 EFFECT OF RESIDUAL STRESSES INDUCED BY PRESTRESSING ON ROLLING-ELEMENT FATIGUE LIFE.	NASA TN D-6996 PREDICTION OF STATIC AERODYNAMIC CHARACTERISTICS FORSPACE-SHUTTLE-LIKE AND OTHER BODIES AT ANGLES OF ATTACK FROM 0 DEGREE TO 180 DEGREE.	NASA TN D-6997 SHOCK WAVES AND DRAG IN THE NUMERICAL CALCULATION OF ISENTROPIC TRANSONIC FLOW.	Next

Bound With Nasa Tn D-6990-93 & 6995-99

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