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THEORY OF HIGHER ORDER OPTIMUM IMPULSIVE SOLUTIONS.

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BookPublisher: National Aeronautics And Space Administration, Washington, D.C. 1971Description: 108.DDC classification: NASA | CR-1847

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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 CR-1847 (Browse shelf)	Not for loan		TR11307

Total holds: 0

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Previous	NASA CR-1837 - EXPERIMENTAL INVESTIGATION OF HIGH AMPLITUDE PANEL FLUTTER	NASA CR-1842 A SHOK WAVE STUDY OF COCONINO SANDSTONE.	NASA CR-1845 THE CALCULATION OF THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERS ON HELICOPTER ROTORS.	NASA CR-1847 THEORY OF HIGHER ORDER OPTIMUM IMPULSIVE SOLUTIONS.	NASA CR-1848 ANALYTICAL PROPERTIES OF NOISE GENERATING MECHANISMS IN A SUPERSONIC JET EXHAUST FLOW.	NASA CR-1849 SENSITIVITY OF THE CREEP-RUPTURE PROPERTIES OF WASPALOY SHEET TO SHARP-EDGED NOTCHES IN THE TEMPERATURE RANGE OF 1000DEGREE TO 1400DEGREE F.	NASA CR-1851 - EXPERIMENTAL STUDY OF ONE-AND TWO-COMPONENT LOW-TURBULENCE CONFINED COAXIAL FLOWS	Next

Bound With Nasa Cr-1841-45,1848-49 Lack No 1843-44,1846

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