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PERFORMANCE OF SEVERAL INLET-BYPASS SYSTEMS FOR MATCHING A TWO-DIMENSIONAL VARIABLE-GEOMETRY MACH 3.0 INLET AT MACH 1.5 AND 2.0

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BookPublisher: Nasa, Washington, D.C. 1959Description: 27.DDC classification: NASA | MEMO 2-6-59E

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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 MEMO 2-6-59E (Browse shelf)	Not for loan Untraceable		TR7378

Total holds: 0

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Previous	NASA MEMO 2-27-59E DETAILS OF EXACT LOW PRANDTL NUMBER BOUNDARY-LAYER SOLUTIONS FOR FORCED AND FOR FREE CONVECTION	NASA MEMO 2-28-59L - COMPARISON OF MEASURED FLAPWISE STRUCTURAL BENDING MOMENTS ON A TEETERING ROTOR BLADE WITH RESULTS CALCULATING FROM THE MEASURED PRESSURE DISTRIBUTION	NASA MEMO 2-5-59E AN EQUATION FOR THE MEAN VELOCITY DISTRIBUTION OF BOUNDARY LAYERS	NASA MEMO 2-6-59E PERFORMANCE OF SEVERAL INLET-BYPASS SYSTEMS FOR MATCHING A TWO-DIMENSIONAL VARIABLE-GEOMETRY MACH 3.0 INLET AT MACH 1.5 AND 2.0	NASA MEMO 2-9-59E AIR- COOLED TURBINE BLADES WITH TIP CAP FOR IMPROVED LEADING-EDGE COOLING	NASA MEMO 3-10-59L JET EFFECTS ON THE BASE PRESSURE OF A CYLINDRICAL AFTERBODY WITH MULTIPLE-JET EXITS	NASA MEMO 3-12-59L THE EFFECT OF LIFT-DRAG RATIO AND SPEED ON THE ABILITY TO POSITION A GLIDING AIRCRAFT FOR A LANDING ON A 5,000-FOOT RUNWAY.	Next

Bound With Nasa Memo 2-5-59e,2-9-59e,2-13-59e-2-27-59e.Lack No Nasa Memo:3-5,7-8,10,12,14-16,18-19,21-22,24,26.

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