NASA Technical Note [D- 3444-59]
By: Washington. National Aeronautics and Space Administration (NASA).
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1966Subject(s): Aeronautics | Spacecraft
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D- 3444-59 | Not for loan | 101086 |
Lack nos. 3446, 3447, 3450, 3455
NASA TN D-3444 -- An experimental study of the oxidation of graphite in high-temperature supersonic and hypersonic environments/ Irvin M. Miller and Kenneth Sutton
NASA TN D-3445 -- Evaluation of special 301-type stainless steel for improved low-temperature notch toughness of cryoformed pressure vessels/ Thomas W. Orange
NASA TN D-3448 -- Energy transport by thermal field emission/ James F. Morris
NASA TN D-3449 -- Effects of subcooling and gravity level on boiling in the discrete bubble region/ Thomas H. Cochran and John C. Aydelott
NASA TN D-3451 -- Prediction of propellant tank pressurization requirements by dimensional analysis/ J. F. Thompson and M. E. Nein
NASA TN D-3452 -- Sets of similarity ratios for thermal modeling/ J. R. Watkins
NASA TN D-3453 -- Mathematical model with experimental verification for the dynamic behavior of a single-tube condenser/ Andrew A. Schoenberg
NASA TN D-3454 -- Effect of face-sheet stiffness on buckling of cylindrical shells of sandwich construction/ Robert E. Fulton and Nancy P. Sykes
NASA TN D-3456 -- Projectile-impact-induced fracture of liquid-filled, filament-reinforced plastic of aluminum tanks/ Francis S. Stepka
NASA TN D-3457 -- Steady-state composition of a low-density nonequilibrium hydrogen plasma/ Roman Krawec
NASA TN D-3458 -- Experimental evaluation of pressurant gas injectors during the pressurized discharge of liquid hydrogen/ Richard L. DeWitt, Robert J. Stochl and William R. Johnson
NASA TN D-3459 -- Effect of thickness and sweep angle on the longitudinal aerodynamic characteristics of slab delta planforms at a mach number of 20/ Robert D. Witcofski and Don C. Marcum
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