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Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 [NASA TN D-839]

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BookSeries: National Aeronautics and space Administratio (NASA). Publisher: Washington, D.C. Nasa 1961Description: 40p.Subject(s): cruciform-wing

Contents:

NASA technical report

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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-839 (Browse shelf)	Not for loan		TR16140

Total holds: 0

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Previous	NASA TN D-836 Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]	NASA TN D-837 Influence of impurity elements, structure, and prestrain on tensile transition temperature of chromium [NASA TN D-837]	NASA TN D-838 Investigation of oxidation-resistant coatings on graphite and molybdenum in two arc-powered facilities [NASA TN D-838]	NASA TN D-839 Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 [NASA TN D-839]	NASA TN D-840 Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configuations at a mach number of 6.83 and angles of attack up to 130 deg [NASA TN D-840]	NASA TN D-882 Stress Concentrations in Filamentary Structures [NASA TN D-882]	NASA TN D-883 Analytical evaluation of a method of midcourse guidance for rendezvous with earth satellites [NASA TN D-883]	Next

NASA technical report

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