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LAMINAR BOUNDARY-LAYER SEPARATION INDUCED BY FLARES ON CYLINDERS WITH HIGHLY COOLED BOUNDARY LAYERS AT A MACH NUMBER OF 15.

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BookPublisher: Nasa, Washington, D.C. Description: 31.DDC classification: NASA | TN D-2601L

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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-2601L (Browse shelf)	Not for loan		TR10881

Total holds: 0

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Previous	NASA TN D-2580 TRANSPORT PROPERTIES OF DILUTE GAS MIXTURES	NASA TN D-2601A AERODYNAMIC CHARACTERISTICS OF LENTICULAR AND ELLIPTIC SHAPED CONFIGURATIONS AT A MACH NUMBERS OF 6.	NASA TN D-2601F FLIGHT-MEASURED WING SURFACE PRESSURES AND LOADS FOR THE X-15 AIRPLANE AT MACH NUMBERS FROM 1.2 TO 6.0	NASA TN D-2601L LAMINAR BOUNDARY-LAYER SEPARATION INDUCED BY FLARES ON CYLINDERS WITH HIGHLY COOLED BOUNDARY LAYERS AT A MACH NUMBER OF 15.	NASA TN D-2601M MARS NONSTOP ROUND-TRIP TRAJECTORIES.	NASA TN D-2601S STRESS-INTENSITY FACTORS FOR SINGLE-EDGE-NOTCH SPECIMENS IN BENDING FOR COMBINED BENDING AND TENSION BY BOUNDARY COLLOCATION OF A STRESS FUCTION	NASA TN D-2601T THERMAL DESIGN AND THERMAL DATA ANALYSIS OF SA-5 PAYLOAD	Next

Bound With Nasa Tn D-2601-2601t

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