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Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Spce Administratio (NASA)Publication details: Nasa, Washington, D.C. 1961Description: 41pSubject(s):

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Technical Note D-974

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR13289 [TN D-974]

Total holds: 0

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Previous	NASA Technical Note [NASA TN D-4517]: A coaxial-flow-stabilized arc	Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having nominal aspect ratios of 3 and 6 [NASA TN D-972]	Effects of gyroscopic cross coupling between pitch and yaw on the handling qualities of vtol aircraft [NASA TN D-973]	Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]	Landing impact - dissipation system [NASA TN D-975]	The smoke-trail method for obtaining detailed measurements of the vertical wind profile for application to missile-dynamic-response problems [NASA TN D-976]	An investigation of effect of downwash from a vtol aircraft and helicopter in the ground environment [NASA TN D-977]	Next

Bound With Nasa Tn D-971-973,975-980

Technical Note D-974

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