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EXPERIMENTAL STUDY OF A SINGLE-COIL INDUCED-ELECTROMOTIVE-FORCE PLASMA ACCELERATOR [NASA TN D-639]

By: Matthews,Clarence W.

Contributor(s): Cuddihy, William F.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Description: 24p.Subject(s): Electromotive force

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 631-640	Not for loan		TR012768 [D-640]

Total holds: 0

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Previous	A WIND-TUNNEL INVESTIGATION OF A TRANSONIC-TRANSPORT CONFIGURATION UTILIZING DRAG-REDUCING DEVICES AT MACH NUMBERS FROM 0.20 TO 1.03 [NASA TN D-636]	WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF WING BODIES, FENCES, FLAPS AND A FUSELAGE ADDITION ON THE WING BUFFET RESPONSE OF A TRANSONIC TRANSPORT MODEL [NASA TN D-637]	ROCKET-MODEL INVESTIGATION OF LATERAL-STABILITY CHARACTERISTICS AND POWER EFFECTS OF A JET-ENGINE AIRPLANE CONFIGURATION WITH TAIL BOOM AT MACH NUMBERS FROM 1.15 TO 1.37 [NASA TN D-638]	EXPERIMENTAL STUDY OF A SINGLE-COIL INDUCED-ELECTROMOTIVE-FORCE PLASMA ACCELERATOR [NASA TN D-639]	Guideance and control payload support requirements for a planetary cartographic probe [NASA TN D-5853]	Full-scale wind-tunnel tests of a nonaarticulated helicopter rotor [NASA TN D-2392] [Bound contains NASA TN D-2391,2393-400]	COUPLED-CHANNELS METHOD FOR REARRANGEMENT COLLISIONS. [NASA TN D-4633]	Next

Bound vol. contains NASA TN D 631-640

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