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AN APPROXIMATE SOLUTION OF ADDITIVE-DRAG COEFFICIENT AND MASS-FLOW RATIO FOR INLETS ULTIZING RIGHT CIRCULAR CONES AT ZERO ANGLE OF ATTACK

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BookPublisher: Nasa, Washington, D.C. 1969Description: 22.DDC classification: NASA | TN D-5537

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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-5537 (Browse shelf)	Not for loan		TR15337

Total holds: 0

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Previous	NASA TN D-5534 THE VISUAL ACUITY IN VIEWING SCALED OBJECTS ON TELEVISION COMPARED WITH THAT IN DIRECT VIEWING	NASA TN D-5535 A STRUCTURAL MERIT FUNCTION FOR AERODYNAMIC DECELERATORS	NASA TN D-5536 ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF END-PLANE ROTATIONS OF TRUNCATED CONES UNDER BENDING LOADS	NASA TN D-5537 AN APPROXIMATE SOLUTION OF ADDITIVE-DRAG COEFFICIENT AND MASS-FLOW RATIO FOR INLETS ULTIZING RIGHT CIRCULAR CONES AT ZERO ANGLE OF ATTACK	NASA TN D-5538 EVALUATION OF A TECHNIQUE FOR DETERMINING AIRPLANE AILERON EFFECTIVENESS AND ROLL RATE BY USING AN AEROELASTICALLY SCALED MODEL	NASA TN D-5539 AN EXTREMELY THIN, OMNIDIRECTIONAL, MICROWAVE ANTENNA ARRAY FOR SACECRAFT APPLICATIONS	NASA TN D-5541 INFINITE PERIODIC MINIMAL SURFACES WITHOUT SELF-INTERSECTIONS	Next

Bound With Nasa Tn D-5530-36,5538-39

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