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A PERFECT-GAS ANALYSIS OF THE EXPANSION TUNNEL, A MODIFICATION TO THE EXPANSION TUBE

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Material type: Text

TextPublication details: Nasa, Washington, D.C. 1965Description: 101DDC 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-223 (Browse shelf(Opens below))	Not for loan		TR14225

Total holds: 0

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Previous	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	NASA TR R-225 ANALYSIS OF THE ERRORS ASSOCIATED WITH THE DETERMINATION OF PLANETARY ATMOSPHERE STRUCTURE FROM MEASURED ACCELERATIONS OF AN ENTRY VEHICLE	NASA TR R-226 A COMPENDIUM OF AEROBEE SOUNDING ROCKET LAUNCHINGS FROM 1959 THROUGH 1963	Next

Bound With Nasa Tr R-221-222,224-230

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