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Aerodynamic design and analysis system for supersonic aircraft [NASA CR-2521] [Bound With NASA CR-2515-2520,Lack No. 2519] : part ii user manual

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Material type: Text

TextLanguage: English Publication details: Washington, D.C. NASA. 1975Description: various pagingsSubject(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		TR13374

Total holds: 0

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Previous	The landing flare [NASA CR-2517] [Bound With NASA CR-2515-2516,2518-2521, Lack No. 2519	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.	Next

Bound With NASA CR-2515-2520,Lack No. 2519

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