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SIMULTANEOUS FILM AND CONVECTION COOLING OF A PLATE INSERTED IN THE EXHAUST STREAM OF A GAS TURBINE COMBUSTOR [NASA TN D-7156]

By: Marek, Cecil J.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1973Description: 34p.Subject(s): Turbine combustors

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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-7150-7159	Not for loan		TR012626

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

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Previous	Evaluation of flow properties behind 120 degree and 140 degree included angle cones and a viking 75 entry vehicle at mach numbers from 1.60 to 3.95	NASA Technical Note [NASA TN D-4450]: Mechanism and kinetics of corrosion of selected iron and cobalt alloys in refluxing mercury	NASA Technical Note [NASA TN D-6299]: Fixed-base simulator investigation of lightweight vehicles for lunar escape to orbit with kinesthetic attitude control and simplified manual guidance	SIMULTANEOUS FILM AND CONVECTION COOLING OF A PLATE INSERTED IN THE EXHAUST STREAM OF A GAS TURBINE COMBUSTOR [NASA TN D-7156]	NEW ASPECTS OF SUBSONIC AERODYNAMIC NOISE THEORY [NASA TN D-7158]	Liquid-filled transsient pressure measuring systems:a method for determining frequency response [NASA TN D-6603]	Effects of thermal and environmental exposure on the mechanical properties of graphite/polyimide composites [NASA TN D-6604]	Next

Bound vol. contains NASA TN D 7150-7159 Lack No. 53

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