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A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at mach numbers of 1.61 and 2.01 for a reflex cambered wind and a cambered and twisted wind having the same swept planform. [NASA TN D-1393]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration (NASA)Publication details: Washington, D.C. 1962 NasaDescription: 70pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		NASA TN D-1393

Total holds: 0

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Previous	Potassium topping cycles for stationary power [NASA CR-2518] [Bound With NASA CR-2515-2517,2520-2521,Lack No. 2519]	Aerodynamic design and analysis system for supersonic aircraft. [NASA CR-2520] [Bound With NASA CR-2515-2518,2521, Lack No. 2519]	Aerodynamic design and analysis system for supersonic aircraft [NASA CR-2521] [Bound With NASA CR-2515-2520,Lack No. 2519]	A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at mach numbers of 1.61 and 2.01 for a reflex cambered wind and a cambered and twisted wind having the same swept planform. [NASA TN D-1393]	sSimulator studies of simple attitude control for spin-stabilized vehicles. [NASA TN D-1395]	AN ANALYTICAL METHOD FOR STUDYING THE LATERAL MOTION OF ATMOSPHERE ENTRY VEHICLES.	NASA TN [D-6553]	Next

Bound With Nasa Tn D-1391-1392,1394-1400.

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