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COMPUTER PROGRAM FOR CALCULATING THE FLOW FIELD OF SUPERSONIC EJECTOR NOZZLES

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1974Description: 86.DDC classification: NASA | TN D-7602

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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-7602 (Browse shelf)	Not for loan		TR13954

Total holds: 0

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Previous	NASA TN D-7599 APOLLO EXPERIENCE REPORT THE COMMAND AND SERVICE MODULE MILESTONE REVIEW PROCESS	NASA TN D-760 - SKID LANDINGS AIRPLANES ON ROCKER -TYPE FUSELAGES	NASA TN D-7601 ASSESSMENT OF AN ANALYTICAL PROCEDURE FOR PREDICTING SUPERSONIC EJECTOR NOZZLE PERFORMANCE	NASA TN D-7602 COMPUTER PROGRAM FOR CALCULATING THE FLOW FIELD OF SUPERSONIC EJECTOR NOZZLES	NASA TN D-7603 A SIMPLIFIED FLIGHT-TEST METHOD FOR DETERMINING AIRCRAFT TAKEOFF PERFORMANCE THAT INCLUDES EFFECTS OF PILOT TECHNIQUE	NASA TN D-7604 THE STRESS CORROSION SUSCEPTIBILITY OF SEVERAL ALLOYS IN HYDRAZINE FUELS	NASA TN D-7606 SONIC-BOOM GROUND PRESSURE MEASUREMENTS FROM THE LAUNCH AND REENTRY OF APOLLO 16	Next

Bound With Nasa Tn D-7600--7601,7603-7610

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