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EFFECT OF BASE BLEED AND TERMINAL FAIRINGS ON THE PERFORMANCE OF EXHAUST-NOZZLE-AFTERBODY COMBINATIONS AT MACH NUMBERS OF 1.93, 2.35, AND 3.05

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BookPublisher: Nasa, Washington, D.C. 1960Description: 31,31.DDC classification: NASA | TN D-539

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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-539 (Browse shelf)	Not for loan		TR16052

Total holds: 0

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Previous	NASA TN D-5385 ANALYSIS OF TOTAL-PRESSURE LOSS AND AIRFLOW DISTRIBUTION FOR ANNULAR GAS TURBINE COMBUSTORS	NASA TN D-5386 EXPERIMENTS ON THE STEADY-STATE CHARACTERISTICS OF HERRINGBONE-GROOVED AIR-LUBRICATED JOURNAL BEARINGS	NASA TN D-5387 GASEOUS-HYDROGEN PRESSURANT REQUIREMENTS FOR THE DISCHARGE OF LIQUID HYDROGEN FROM A 3.96-METER- (13-FT-) DIAMETER SPHERICAL TANK	NASA TN D-539 EFFECT OF BASE BLEED AND TERMINAL FAIRINGS ON THE PERFORMANCE OF EXHAUST-NOZZLE-AFTERBODY COMBINATIONS AT MACH NUMBERS OF 1.93, 2.35, AND 3.05	NASA TN D-5390 EFFECT OF STRESS RATIO ON FATIGUE-CRACK GROWTH IN 7075-T-6 AND 2024-T-3 ALUMINUM-ALLOY SPECIMENS [NASA TN D-5390]	NASA TN D-540 EFFECTS OF FINENESS RAIO AND REYNOLDS NUMBER ON THE LOW-SPEED CROSSWIND DRAG CHRACTERISTICS OF CIRCULAR AND MODIFUED-SQUARE CYLINDERS	NASA TN D-5408 STATIC AND DYNAMIC STABILITY DERIVATIVES OF A MODEL OF A JET TRANSPORT EQUIPPED WITH EXTERNAL-FLOW JET -AUGMENTED FLAPS	Next

Bound With Nasa Tn D-531-538,540.

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