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EFFECT OF WING SWEEP, ANGLE OF ATTACK, REYNOLDS NUMBER, AND WING ROOT FILLET ON THE INTERFERENCE HEATING TO THE WING WINDWARD SURFACE OF AN ENTRY VEHICLE CONFIGURATION

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BookPublisher: NASA, WASHINGTON, D.C. 1972Description: ,52.DDC classification: NASA | TN D-7060

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-7060 (Browse shelf)	Not for loan		101296

Total holds: 0

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Previous	NASA TN D-7030 Boundary layer measurements in an accelerated flow with and without heat transfer [NASA TN D-7030--TN D-7039]	NASA TN D-7032 - ALLMAT	NASA TN D-7033 - ROLLING-ELEMENT FATIGUE LIVES OF FOUR M-SERIES STEELS AND AISI 52100 AT 150(DEGREE)F	NASA TN D-7060 EFFECT OF WING SWEEP, ANGLE OF ATTACK, REYNOLDS NUMBER, AND WING ROOT FILLET ON THE INTERFERENCE HEATING TO THE WING WINDWARD SURFACE OF AN ENTRY VEHICLE CONFIGURATION	NASA TN D-7070 EXPERIMENTAL PERFORMANCE OF AN INTERNAL RESISTANCE HEATER FOR LANGLEY 6-INCH EXPANSION TUBE DRIVER.	NASA TN D-7080 APPOLO EXPERIENCE REPORT PROTECTION AGAINST RADIATION	NASA TN D-7110 MINIMIZING THE AREA REQUIRED FOR TIME CONSTANTS IN INTEGRATED CIRCUITS	Next

Bound with NASA TN D-7061-7069

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