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Turbine aerodyanamics and cooloing requirements for a turbojet powered mach 3 transport ising mehane fuel [NASA TN D-5928]

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BookPublisher: Washington, D. C. NASA August 1970Description: 78p.

Contents:

NASA TN D-5928 NASA TECHNICA NOTE

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference		Not for loan		TR012167

Total holds: 0

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Previous	Transient characteristics of a voltageregulator and a parastic speed controller on a 14.3-Kilovolt-amplifier, 1200-Hertz modified lundell alternator [NASA TN D-5925]	Effects of termal loading on composites with constituents os diffffering thermal expansion [NASA TN D-5926]	p-p and p-t final interaction 3HE9d, tp)p NASA TN D -5927	Turbine aerodyanamics and cooloing requirements for a turbojet powered mach 3 transport ising mehane fuel [NASA TN D-5928]	Block and strip solutions involving lunar orbiter photographic data used to preprecontour charts for five apollo landing sites [NASA TN D-5929]	An electronioc striain level conunter for aircraft structuctural members [NASA TN D-5944]	Numerila integration of orbits in mutirevolution steps [NASA TN D-5915]	Next

NASA TN D-5928
NASA TECHNICA NOTE

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