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A mixing model for rocket engine combustion [NASA TN D-2881]

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Material type: Text

TextLanguage: English Series: National Aeronautics And Space Administration [NASA]Publication details: Washington, D. C. NASA 1965Description: 24pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA TN D-2881 (Browse shelf(Opens below))	Not for loan		64289

Total holds: 0

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Previous	NASA TN D-2479 Effect of store pitch flexibility on flutter characteristics of a wing-store configuration at mach numbers near 0.85	NASA TN D-2480 Measurements of efflux patterns and flow rates from cylindrical tubes in free-molecule and slip flows	NASA TN D-2871 Free-flight measurements of stagnation-point convective heat transfer at velocities to 41,00 FT/SEC [NASA TN D-2871]	NASA TN D-2881 A mixing model for rocket engine combustion [NASA TN D-2881]	NASA TN D-2882 Ionosphere topside sounder studies I-the reduction of alouette I ionograms to electron density profiles [NASA TN D-2882]	NASA TN D-2887 Experimental study of wind-tunnel wall effects and wall corrections for a general-research V/Stol tilt-wing model with flap [NASA TN D-2887]	NASA TN D-2888 Extragalactic radio sources [NASA TN D-2888]	Next

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