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EFFECTS OF RADIAL AND CIRCUMFERRENTIAL INLET VELOCITY PROFILE DISTORTIONS ON PERFORMANCE OF A SHORT-LENGHTH DOUBLE-ANNULAR RAM-INDUCATION COMBUSTORS.

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BookPublisher: Nasa, Washington, D.C. 1972Description: 40.DDC classification: NASA | TN D-6706

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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-6706 (Browse shelf)	Not for loan		TR15772

Total holds: 0

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Previous	NASA TN D-6703 EVAULATION OF THE USE OF A SINGULARITY ELEMENT IN FIFNITE-ELEMENT ANALYSES OF CENTER-CRACKED PLATES.	NASA TN D-6704 ELECTROTHERMAL OSCILLATIONS AND TEH QUASI-LINEAR THEORY OF ELECTRON ENTHALPY FLUCATIONS IN MAGNETOHYDRODENAMIC GENERATIORS IAND MAGNETOPLASMADYNAMIC ARC THRUSTERS.	NASA TN D-6705 THURST MEASUREMENTS OF A HOLLLOW-CATHODE DISCHARGE.	NASA TN D-6706 EFFECTS OF RADIAL AND CIRCUMFERRENTIAL INLET VELOCITY PROFILE DISTORTIONS ON PERFORMANCE OF A SHORT-LENGHTH DOUBLE-ANNULAR RAM-INDUCATION COMBUSTORS.	NASA TN D-6707 OPTIMAL CRUSE TRAJETORIES FOR SUPERSONIC AIRPLANES.	NASA TN D-6708 STATISTICAL ANALYSIS OF LANDING CONTACT CONDITIONS FOR THREE LIFTING BODY RESEARCH VEHICLES.	NASA TN D-6709 DESIGN OF RECURSIVE DIGITAL FILTERS HAVING SPECIFIED PHASE AND MAGNITUDE CHARATERISTICS.	Next

Bound With Nasa Tn D-6700-6706,6708-6719.Lack No-6701-6702

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