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AN ANALYTICAL METHOD FOR STUDYING THE LATERAL MOTION OF ATMOSPHERE ENTRY VEHICLES.

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Material type: Text

TextPublication details: Nasa, Washington, D.C. 1960Description: 17DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 321-330	Not for loan		TR16085

Total holds: 0

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Previous	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]	NASA TN [D-6556]	NASA TN [D-6557]	Next

Bound With Nasa Tn D-321-324,326-330.

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