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Low-speed longitudinal chracteristics of an airplane configuration including effects of canard and wing trailing-edge flap controls in combination[NASA TN D-1397]

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BookSeries: National aeronautics and space administration (NASA). Publisher: Washington, D.C. 1962Description: 47p.Subject(s): Low-speedDDC classification: NASA | TN D-1397

Contents:

NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-1397 (Browse shelf)	Not for loan		TR13015

Total holds: 0

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Previous	NASA TN D-1311 Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms	NASA TN D-1394 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]	NASA TN D-1396 An analysis of the coning motions of the final stages of three nasa scout development vehicles [NASA TN D-1396]	NASA TN D-1397 Low-speed longitudinal chracteristics of an airplane configuration including effects of canard and wing trailing-edge flap controls in combination[NASA TN D-1397]	NASA TN D-1398 A study of thrust vector steering for rendezvous with a near-earth satellite utilizing athree-stage vehicle launched out of the satellite plane [NASA TN D-1398]	NASA TN D-1399 Effect of a afterbody-ejector configurations on the performance at transonic speeds[NASA TN D-1399]	NASA TN D-1400 Induced interference effects on a four-jet vtol configuration with various wing planforms in the transition speeds range[NASA TN D-1400]	Next

Bound With Nasa Tn D-1391-1396,1398-1400.

NASA technical report

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