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General solution of the laminar compressible boundary layer in the stagnation region of blunt bodies in axisymmetric flow. [NASA TN D- 2234]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1964Description: 168p.Subject(s): Laminar

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NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-2234 (Browse shelf)	Not for loan		TR13555

Total holds: 0

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Previous	NASA TN D-2231 Flight investigation of the performance,handling qualities, and operational characteristics of a deflected slipstream stol transport airplane having four interconnected propellers. [NASA TN D-2231]	NASA TN D-2232 Impact flash at flow ambient pressures [NASA TN D-2232]	NASA TN D-2233 The total enthalpy of a one-dinesional nozzel flow with various gases [NASA TN D-2233]	NASA TN D-2234 General solution of the laminar compressible boundary layer in the stagnation region of blunt bodies in axisymmetric flow. [NASA TN D- 2234]	NASA TN D-2235 Sputtering at oblique angles of ion incidence [NASA TN D-2235]	NASA TN D-2281 RESEARCH ON RESISTANCE-HEATED HYDROGEN THRUSTORS	NASA TN D-2369 EFFECT OF INERCHANGING PROPELLANTS ON ROCKET COMBUSTOR PERFORMANCE WITH COAXIAL INJECTION.	Next

NASA technical report

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