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Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) (NASA technical memorandum)

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Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) (NASA technical memorandum)

Daniel J Gauntner

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Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) (NASA technical memorandum)

Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) (NASA technical memorandum)

More Books

Method for calculating convective heat-transfer coeffecients over turbine vane surfaces / Daniel J. Gauntner and James Sucec. 1978 [Leather Bound]

Method for calculating convective heat-transfer coeffecients over turbine vane surfaces / Daniel J. Gauntner and James Sucec. 1978 [Leather Bound]

Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) / by Daniel J. Gauntner and Albert Kaufman. [Leather Bound]

Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) / by Daniel J. Gauntner and Albert Kaufman. [Leather Bound]