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EFFECT OF REYNOLDS NUMBER ON OVERALL PERFORMANCE OF A 3.7-INCH-DIAMETER SIX-STAGE AXIAL-FLOW COMPRESSOR

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BookPublisher: Nasa, Washington, D.C. 1972Description: 20.DDC classification: NASA | TN D-6628

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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 TN D-6628 (Browse shelf)	Not for loan		TR15154

Total holds: 0

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Previous	NASA TN D-6625 EFFECTS OF NORMAL ACCELERATION ON TRANSIENT BURNING-RATE AUGMENTATION OF AN ALUMINIZED SOLID PROPELLANT	NASA TN D-6626 DIMENSIONAL-STABILITY STUDIES OF CANDIDATE SPACE-TELESCOPE MIRROR-SUBSTRATE MATERIALS	NASA TN D-6627 WIND-TUNNEL STUDY OF SLOT SPOILERS FOR DIRECT LIFT CONTROL	NASA TN D-6628 EFFECT OF REYNOLDS NUMBER ON OVERALL PERFORMANCE OF A 3.7-INCH-DIAMETER SIX-STAGE AXIAL-FLOW COMPRESSOR	NASA TN D-6629 DEFINITION AND APPLICATION OF LONGITUDINAL STABILITY DERIVATIVES FOR ELASTIC AIRPLANES	NASA TN D-6631 - EFFECTS OF 22-MEV PROTONS ON SINGLE JUNCTION AND SILICON CONTROLLED RECTIFIERS	NASA TN D-6632 - SHORT-TERM HOT HARDNESS CHARACTERISTICS OF ROLLING-ELEMENT STEELS	Next

Bound With Nasa Tn D-6620-6627,,6629

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