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COMUSTION STABILITY OF SINGLE SWIRL-CAN COMBUSTOR MODULES USING ASTM-AI LIQUID FUEL.

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BookPublisher: Nasa, Washington, D.C. 27Description: 27.DDC classification: NASA | TN D-5436

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-5436 (Browse shelf)	Not for loan		TR15176

Total holds: 0

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Previous	NASA TN D-5433 COPMARISION OF PREDICATION METHODS AND STUDIES OF RELAXATION IN HYPERSONIC TURBULENT NOZZLE-WALL BOUNDARY LAYERS.	NASA TN D-5434 A MODIFIED METHOD OF INTEGRAL RELATIONS APPROACH TO THE BLUNT-BODY EQULIBRIUM AIR FLOW FIELD,INCLUDIND COMPARISONS WITH INVERSE SOLUTIONS.	NASA TN D-5435 THE INFLUENCE OF THERMAL DISTORTION ON THE PERFORMANCE OF GRAVITY-STABILIZED SATELLITES.	NASA TN D-5436 COMUSTION STABILITY OF SINGLE SWIRL-CAN COMBUSTOR MODULES USING ASTM-AI LIQUID FUEL.	NASA TN D-5437 A COPUTER PROGRAM FOR COMPOSING COMPRESSOR BLADING FROM SIMULATED CIRCULAR-ARC ELEMENTS ON CONICAL SURFACE.	NASA TN D-5438 BODIES OF REVOLATION HAVING MINIMUM TOTAL DRAG IN HYPERSONIC FLOW.	NASA TN D-5439 FINAL REPORT	Next

Bound With Nasa Tn D-5421-5435.5437-5440.Lack No-5427

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