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ANALYSIS OF HEAT-TRANSFER EFFECTS IN ROCKET NOZZLES OPERATING WITH VERY HIGH-TEMPERATURE HYDROGEN.

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Material type: Text

TextPublication details: Nasa, Washington, D.C. Description: 32DDC classification:

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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	General Stacks	NASA TR R-220 (Browse shelf(Opens below))	Not for loan		TR11759

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	NASA TR R-217 LIOUVILLE'S EQUATION AND THE N-BODY PROBLEM.	NASA TR R-218 POLARIZATION OF PROTONS FROM (D,P) REACTIONS AT 21 MEV.	NASA TR R-219 CHARACTERISTICS OF A CONTINUOUS-FLOW INDUCTION PLASMA ACCELERATOR.	NASA TR R-220 ANALYSIS OF HEAT-TRANSFER EFFECTS IN ROCKET NOZZLES OPERATING WITH VERY HIGH-TEMPERATURE HYDROGEN.	NASA TR R-222 EQUATIONS FOR ISENTROPIC AND PLANE SHOCK FLOWS OF MIXTURES OF UNDISSOCIATED PLANETARY GASES	NASA TR R-223 A PERFECT-GAS ANALYSIS OF THE EXPANSION TUNNEL, A MODIFICATION TO THE EXPANSION TUBE	NASA TR R-224 CONVECTIVE HEAT TRANSFER IN PLANETARY GASES	Next

Bound With Nasa Tr R-211-219

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