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DYNAMIC RESPONSE OF MACH 2.5 AXISYMMETRIC INLET WITH ENGINE OR COLD PIPE AND UTILIZING 60 PERCENT SUPERSONIC INERNAL AREA CONTRACTION.

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BookPublisher: Nasa, Washington, D.C. 1969Description: 58.DDC classification: NASA | TN D-5338

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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-5338 (Browse shelf)	Not for loan		TR10457

Total holds: 0

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Previous	NASA TN D-5335 A FINITE-STEP METHOD FOR CALCULATION OF THEORETICAL LOAD DISTRIBUTIONS FOR ARBITRARY LIFTING-SURFACE ARRANGEMENTS AT SUBSONIC SPEEDS.	NASA TN D-5336 GASEOUS-HYDROGEN REQUIREMENTS FOR THE DISCHARGE OF LIQUID HYDROGEN FROM A 1.52-METER-(5-FT-) DIAMETER SPHERICAL TANK	NASA TN D-5337 INERCOMPARISON OF THE MINITRACK AND OPTICAL TRACKING NETWORKS USING GEOS 1 LONG-ARC ORBITAL SOLUTIONS.	NASA TN D-5338 DYNAMIC RESPONSE OF MACH 2.5 AXISYMMETRIC INLET WITH ENGINE OR COLD PIPE AND UTILIZING 60 PERCENT SUPERSONIC INERNAL AREA CONTRACTION.	NASA TN D-5339 ABALYSIS OF THE DYNAMIC RESPONSE OF LIQUID ATOMIZATION TO ACOUSTIC OSCILLATIONS	NASA TN D-534 HOVERING MEASUREMENTS FOR TWIN-ROTOR CONFIGURATIONS WITH ANDF WITHOUT OVERLAP.	NASA TN D-5340 A SEMIEMPIRICAL FRACTURE ANALYSIS FOR SMALL SURFACE CRACKS.	Next

Bound With: Nasa Tn D-5331-5337,5339-5340

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