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Experimental and theoretical turbulent boundary layer development in a mach 4.4 water cooled conical nozzle [NASA TN D-5377]

By: Boldman, Donald R.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D. C. National Aeronautics and Space Administration 1969Description: 41p.Subject(s): Conical nozzle

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 5371-5380	Not for loan		TR009341

Total holds: 0

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Previous	Causes measurement and elimination of fuel element fission product leakage at the NASA plum brook reactor [NASA TN D-5374]	Effect of injection element radial distribution and chamber geometry on acoustic mode instability in a hydrogen oxygen rocket [NASA TN D-5375]	Oxidation and thermal fatigue cracking of nickel and cobalt base alloys in a high velocity gas stream [NASA TN D-5376]	Experimental and theoretical turbulent boundary layer development in a mach 4.4 water cooled conical nozzle [NASA TN D-5377]	Aerodynamic charectristics in pitch of a 1/7 scale model of a two of a two and three stage rocket configuration at mach numbers of 0.4 to 4.63 [NASA TN D-5378]	Aerodynamics interference effects caused by parellel staged simple aerdynamic configurations at mach numbers of 3 and 6 [NASA TN D-5379]	Molecular orientation and mechanical anisotropy in polypropylene and poly (ethylene terephthalate) films [NASA TN D-5380]	Next

Bound vol. contains NASA TN D 5371-5380

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