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PERFORMANCE OF SHORT LENGTH TURBOJET COMBUSTOR INSENSITIVE TO RADIAL DISTORTION OF INLET AIRFLOW

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BookPublisher: NASA, WASHINGTON, D.C. 1970Description: ,37.DDC classification: NASA | TN D-5570

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-5570 (Browse shelf)	Not for loan		101176

Total holds: 0

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Previous	NASA TN D-5510 HOT-SALT STRESS-CORROSION OF A TITANIUM ALLOY UNDER A SIMULATED TURBINE-ENGINE COMPRESSOR ENVIRONMENT	NASA TN D-5520 CONVECTIVE HEAT-TRANSFER COEFFICIENTS FROM A SOLUTION OF THE CONDUCTION EQUUATION FOR A WALL SEPRATING TWO FLUIDS, ONE HAVING AN OSCILLATING TEMPERATURE.	NASA TN D-5530 INTERACTION OF 42-MEV ALPHA PARTICLES WITH HELIUM-3	NASA TN D-5570 PERFORMANCE OF SHORT LENGTH TURBOJET COMBUSTOR INSENSITIVE TO RADIAL DISTORTION OF INLET AIRFLOW	NASA TN D-5590 AN AUTOMATIC RESTART CONTROL SYSTEM FOR AN AXISYMMETRIC MIXED-COMPRESSION INLET.	NASA TN D-5600 AERODYNAMIC CHARACTERISTICS OF AN OBLATE SPHEROID AND A SPHERE AT MACH NUMBERS FROM 1.70 TO 10.49	NASA TN D-5611 - PASSIVE METHOD FOR SCANNING THE CELESTIAL SPHERE	Next

Bound with NASA TN D-5571-79

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