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EQUATIONS FOR THE APPLICATION OF WIND-TUNNEL WALL CORRECTIONS TO PITCHING MOMENTS CAUSED BY THE TAIL OF AN AIRCRAFT MODEL.

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BookPublisher: Nasa, Washington, D.C. Description: 18.DDC classification: NASA | TN D-3738

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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-3738 (Browse shelf)	Not for loan Untraceable		TR12250

Total holds: 0

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Previous	NASA TN D-3735 PARAMETRIC STUDY OF A LOW-DENSITY CHARRING ABLATOR.	NASA TN D-3736 HEAT-TRANSFER MEASUREMENTS ON A FLAT PLATE WITH ATTACHED PROTUBERANCES IN A TURBULENT BOUNDARY LAYER AT MACH NUMBERS OF 2.49,3.51,AND 4.44.	NASA TN D-3737 REMARKS ON PRACTICAL SPECTROSCOPIC TEMPERATURE MEASUREMENTS IN PLASMAS.	NASA TN D-3738 EQUATIONS FOR THE APPLICATION OF WIND-TUNNEL WALL CORRECTIONS TO PITCHING MOMENTS CAUSED BY THE TAIL OF AN AIRCRAFT MODEL.	NASA TN D-3739 JUPITER HIGH-THRUST ROUND-TRIP TRAJECTORIES.	NASA TN D-374 EFFECTS OF VARIOUS AGINE HEAT TREATMENTS AND SOLUTION-ANNEALING AND AGINE HEAT TREATMENTS ON TENSILE, CREEP, AND STRESS-RUPTURE STRENGTHS OF INCONEL X SHEET TO TEMPERATURES OF 1,400 DEGREE F	NASA TN D-3740 A STUDY OF ARTIFICIAL METEORS AS ABLATORS.	Next

Bound With Nasa Tn D-3731-37, 3739-40

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