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A THEORETICAL TREATMENT OF THE STEADY-FLOW,LINEAR,CROSSED-FIELD,DIRECT-CURRENT PLASMA ACCELERATOR FOR INVISCID,ADIABATIC,ISOTHERMAL, CONSTANT-AREA FLOW

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BookPublisher: Nasa, Washington, D.C. 1961Description: 19.DDC classification: NASA | TR R-114

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TR R-114 (Browse shelf)	Not for loan		TR13996

Total holds: 0

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Previous	NASA TR R-110 ANALYTICAL METHOD OF APPROXIMATING THE MOTION OF A SPINNING VEHICLE WITH VARIABLE MASS AND INERTIA PROPERTIES ACTED UPON BY SEVERAL DISTURBING PARAMETERS	NASA TR R-112 A METHOD FOR THE CALCULATION OF LATTICE ENERGIES OF COMPLEX CRYSTALS WITH APPLICATION TO THE OXIDES OF MOLYBDENUM	NASA TR R-113 STUDY OF STATISTICAL DATA-ADJUSTMENT AND LOGIC TECHNIQUES AS APPLIED TO THE ITERPLANETARY MIDCOURSE GUIDANCE PROBLEM	NASA TR R-114 A THEORETICAL TREATMENT OF THE STEADY-FLOW,LINEAR,CROSSED-FIELD,DIRECT-CURRENT PLASMA ACCELERATOR FOR INVISCID,ADIABATIC,ISOTHERMAL, CONSTANT-AREA FLOW	NASA TR R-115 METHOD FOR APPROXIMATING THE VACUUM MOTIONS OF SPINNING SYMMETRICAL BODIES WITH NONCONSTANT SPIN RATES	NASA TR R-116 NUMERICAL PREDICTIONS OF RADIATIVE INTERCHANGE BETWEEN CONDUCTING FINS WITH MUTUAL IRRADIATIONS	NASA TR R-117 TURBULENT BOUNDARY-LAYER SEPARATION INDUCED BY FLARES ON CYLINDERS AT ZERO ANGLE OF ATTACK	Next

Bound With Nasa Tr R-111-113,115-120

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