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Investigation of net-thurst and base-pressure characterstics of cylindrical afterbodies with clustered super sonic nozzles at transonic mach numbers [NASA TN D-978]

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Material type: Text

TextLanguage: English Series: National Aeronautics and space AdministrationPublication details: Nasa 1961 Washington, D.C.Description: 46pSubject(s):

Contents:

Technical Note D-978

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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		TR13293 [ TN D-978]

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	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]	Guidance and control during direct-descent parabolic reentry [NASA TN D-979]	Estimates of minimum energy requirements for range-controlled return of a nonlifting satellite from a circular orbit [NASA TN D-980]	NASA TN [D-5671]	Next

Bound With Nasa Tn D-971-977,979-980

Technical Note D-978

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