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A TIME DEPENDENT METHOD FOR CALCULATING SUPERSONIC BLUNT-BODY FLOW FIELDS WITH SHARP CORNERS AND EMBEDDED SHOCK WAVES

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Material type: Text

TextPublication details: Nasa, Washington, D.C. 1970Description: 65DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TND-6031 - (Browse shelf(Opens below))	Not for loan		TR8319

Total holds: 0

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Previous	NASA TND-5982 - SIMULATION STUDY OF THREE INSTRUMENT DISPLAYS TO ASSIST IN AIRPLANE THRUST MANAGEMENT	NASA TND-5983 - FIXED-BASE VISUAL-SIMULATION STUDY OF MANUALLY CONTROLLED OPERATION OF A LUNAR FLYING VEHICLE	NASA TND-5984 - THEORETICAL PRESSURE DISTRIBUTIONS OVER ARBITRARILY SHAPED PERIODIC WAVES IN SUBSONIC COMORESSIBLE FLOW AND COMPARISON WITH EXPERIMENT	NASA TND-6031 - A TIME DEPENDENT METHOD FOR CALCULATING SUPERSONIC BLUNT-BODY FLOW FIELDS WITH SHARP CORNERS AND EMBEDDED SHOCK WAVES	NASA TND-6032 - EVALUTION RESULT AND ACCURACY IMPROVEMENT OF TWO FLUX-SWITCHING MATHEMATICAL MODELS FOR MAGNETIC CORES	NASA TND-7373 - APOLLO EXPERIENCE REPORT THE DEVELOPMENT OF DESIGN-LOADS CRITERIA,METHODS AND OPERATIONAL PROCEDURES FOR PRELAUNCH,LIFT-OFF AND MIDBOOST CONDITIONS	NASA TND-7374 - APOLLO EXPERIENCE REPORT -COMMAND AND SERVICE MODULE INSTRUMENTATION SUBSYSTEM	Next

Bound With Nasa Tnd-6030

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