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EXPERIMENTAL INVESTIGATION OF METAL TEMPERATURES OF AIR-COOLED AIRFOIL LEADING EDGES AT SUBSONIC FLOW AND GAS TEMPERATURES UP TO 2780(DEGRE) F

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BookPublisher: Nasa, Washington, D.C. 1959Description: 32.DDC classification: NASA | TN D-127

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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-127 (Browse shelf)	Not for loan		TR15635

Total holds: 0

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Previous	NASA TN D-1267 CURRENT ESTIMATES OF RADIATION DOES IN SPACE	NASA TN D-1268 MEASUREMENT OF TOTAL NORMAL EMITTANCE OF BORON NITRIDE FROM 1,200 (DEGRE) F TO 1,900 (DEGRE) F WITH NORMAL SPECTRAL EMITTANCE DATA AT 1,400 (DEGRE) F	NASA TN D-1269 IMPACT CHARACTERISTICS OF VARIOUS MATERIALS OBTAINED BY AN ACCELERATION-TIME-HISTORY TECHNIQUE APPLICABLE TO EVALUATING REMOTE TARGETS	NASA TN D-127 EXPERIMENTAL INVESTIGATION OF METAL TEMPERATURES OF AIR-COOLED AIRFOIL LEADING EDGES AT SUBSONIC FLOW AND GAS TEMPERATURES UP TO 2780(DEGRE) F	NASA TN D-1270 THE GRAVITATIONAL FIELD ENVIRONMENT OF AN EARTH SATELLITE	NASA TN D-1272 AERODYNAMIC CHARACTERISTICS IN PITCH OF SEVERAL RING-WING-BODY CONFIGURATIONS AT A MACH NUMBER OF 2.2	NASA TN D-1273 CONCEPTUAL DESIGN STUDY OF A MULTIPURPOSE AEROSPACE TEST FACILITY	Next

Bound With Nasa Tn D-121-126,128-130

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