Normal view MARC view ISBD view

Landing impact - dissipation system [NASA TN D-975]

By:

Material type: Text

TextLanguage: English Series: National Aeronautics and Spce Administratio (NASA)Publication details: Nasa 1961 Washington, D.C.Description: 25pSubject(s):

Contents:

Technical Note D-975

Average rating: 0.0 (0 votes)

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		TR13290 [TN D-975]

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	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]	Investigation of net-thurst and base-pressure characterstics of cylindrical afterbodies with clustered super sonic nozzles at transonic mach numbers [NASA TN D-978]	Next

Bound With Nasa Tn D-971-974,976-980

Technical Note D-975

There are no comments on this title.

to post a comment.

Welcome to P K Kelkar Library, Online Public Access Catalogue (OPAC)