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WIND-TUNNEL CALIBRATIONS OF A COMBINED PITOT-STATIC TUBE, VANE-TYPE FLOW -DIRECTION TRANSMITTER, AND STAGNATION-TEMPERATURE ELEMENT AT MACH NUMBERS FROM 0.60 TO 2.87

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BookPublisher: Nasa, Washington, D.C. 1959Description: 26.DDC classification: NASA | TN D-122

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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-122 (Browse shelf)	Not for loan		TR15630

Total holds: 0

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Previous	NASA TN D-1216 - STUDY OF A SINUSOIDALLY PERTURBED FLOW IN A LINE INCLUDING A 90(DEGREE) ELBOW WITH FLEXIBLE SUPPORTS	NASA TN D-1218 - MEASUREMENTS OF FLOW DURATION IN A LOW PRESSURE SHOCK TUBE	NASA TN D-1219 - COMPARATIVE MEASUREMENTS OF SINGLY AND DOUBLY IONIZED MERCURY PRODUCED BY ELECTRON BOMBARDMENT ION ENGINE	NASA TN D-122 WIND-TUNNEL CALIBRATIONS OF A COMBINED PITOT-STATIC TUBE, VANE-TYPE FLOW -DIRECTION TRANSMITTER, AND STAGNATION-TEMPERATURE ELEMENT AT MACH NUMBERS FROM 0.60 TO 2.87	NASA TN D-1220 - STABILITY OF THREE-DIMENSIONAL COMPRESSIBLE BOUNDARY LAYERS	NASA TN D-1222 ELECTRODE CONFIGURATIONS FOR A WIND-TUNNEL HEATER INCORPORATING THE MAGNETICALLY SPUN ELECTRIC ARC	NASA TN D-1223 A THEORETICAL INVESTIGATION OF THE EFFECT OF CROSS-CONTROL DEVIVATIVES ON THE STABILITY CHARACTERISTICS OF AIRPLANES DESIGNED FOR FLIGHT	Next

Bound With Nasa Tn D-121,123-130

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