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SUBSONIC WIND-TUNNEL TESTS OF A TRAILING-CONE DEVICE FOR CALIBRATING AIRCRAFT STATIC-PRESSURE SYSTEM

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BookPublisher: Nasa, Washington, D.C. 1973Description: 25.DDC classification: NASA | TN D-7217 -

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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-7217 - (Browse shelf)	Not for loan		TR10249

Total holds: 0

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Previous	NASA TN D-7214 - ANALYSIS OF TEMPERATURE-DEPENDENT NEUTRON TRANSMISSION AND SELF-INDICATION MEASUREMENTS ON TANTALUM AT 2-KEV NEUTRON ENERGY	NASA TN D-7215 - SOME EFFECTS OF GROOVED RUNWAY CONFIGURATIONS ON AIRCRAFT TIRE BRAKING TRACTION UNDER FLOODED RUNWAY CONDITIONS	NASA TN D-7216 - RESULTS OF THE NOISE MEASUREMENT PROGRAM ON A STANDARD AND MODIFIED OH-6A HELICOPTER	NASA TN D-7217 - SUBSONIC WIND-TUNNEL TESTS OF A TRAILING-CONE DEVICE FOR CALIBRATING AIRCRAFT STATIC-PRESSURE SYSTEM	NASA TN D-7218 - APPLICATION OF SONIC-BOOM MINIMIZATION CONCEPTS IN SUPERSONIC TRANSPORT DESIGN	NASA TN D-7219 - HEAT PIPE INVESTIGATIONS	NASA TN D-7221 - Material selection method based on material properties and operating parameters	Next

Bound With Nasa Tn D-7211-19

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