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AN INVESTIGATION OF SPLITTER PLATES FOR THE AERODYNAMIC SEPARATION OF TWIN INLETS AT MACH 2.5

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BookPublisher: Nasa, Washington, D.C. 1966Description: 50.DDC classification: NASA | TN D-3385

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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-3385 (Browse shelf)	Not for loan		TR13058

Total holds: 0

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Previous	NASA TN D-3382 EFFECT OF REDUCED COMPUTER PRECISION ON A MIDCOURSE NAVIGATION AND GUIDANCE SYSTEM USING OPTIMAL FILTERING AND LINEAR PREDICTION	NASA TN D-3383 NUMERICAL SOLUTIONS FOR BLUNT AXISYMMETRIC BODIES IN A SUPERSONIC SPHERICAL SOURCE FLOW	NASA TN D-3384 A REVIEW OF FACTORS AFFECTING BOUNDARY-LAYER TRANSITION	NASA TN D-3385 AN INVESTIGATION OF SPLITTER PLATES FOR THE AERODYNAMIC SEPARATION OF TWIN INLETS AT MACH 2.5	NASA TN D-3386 SUMMARY OF HIGH-ALTITUDE AND ENTRY FLIGHT CONTROL EXPERIENCE WITH THE X-15 AIRPLANE	NASA TN D-3387 A GENERAL MATHEMATICAL MODEL FOR BEAM AND PLATE VIBRATION LUMPED PARAMETERS	NASA TN D-3388 EFFECTS OF BLUNTNESS ON THE SUBSCONIC DRAG OF AN ELLIPTICAL FOREBODY	Next

Bound With Nasa Tn D-3381-84,3386-90

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