NASA Technical Memorandum [X- 2916-92 & 2641]
By: Washington. National Aeronautics and Space Administration (NASA).
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Memorandum. Publisher: Washington NASA 1974Subject(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 TM X- 2916-92 & 2641 | Not for loan | 102493 |
Lack No.: 2917, 20-40, 42-50, 52-62, 65-66, 68, 70-72, 74-80, 82, 84, 87-91
NASA TM X-2916 – Transient response of shells of revolution by direct integration and modal superposition methods/ Wendell B. Stephens and Howard M. Adelman
NASA TM X-2918 – Flight velocity effects on jet noise of several variations of a twelve-chute suppressor installed on a plug nozzle/ Richard R. Burley and Albert L. Johns
NASA TM X-2919 – Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle/ Richard R. Burley and Verlon L. Head
NASA TM X-2641 – An annotated bibliography of Pyrrone and BBB publications/ Harold D. Burks
NASA TM X-2951 – Thrust performance of isolated plug nozzles with two types of 40-spoke noise suppressor at mach numbers from 0 to 0.45/ Douglas E. Harrington and James J. Schloemer
NASA TM X-2963 – Compatibility of refractory materials for nuclear reactor poison control systems/ John H. Sinclair
NASA TM X-2964 – Tensile properties from room temperature to 1315 [degree] C of tungsten-lined tantalum-alloy (T-111) tubing fabricated by hot isostatic pressing/ Robert J. Buzzard and Robert R. Metroka
NASA TM X-2967 – Fortran program to generate engine inlet flow contour maps and distortion parameters/ John H. Dicus
NASA TM X-2969 – Effect of chromia doping on thermal stability of silica fibers/ Isidor Zaplatynsky
NASA TM X-2973 – Forward-slanted slot throat stability bypass to increase the stable airflow range of a mach 2.5 inlet with 60-percent internal contraction/ Robert J. Shaw, Glenn A. Mitchell and Bobby W. Sanders
NASA TM X-2981 – Off-design temperature effects on nuclear fuel pins for an advanced space-power-reactor concept/ Kenneth J. Bowles
NASA TM X-2983 – Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle/ Verlon L. Head
NASA TM X-2985 – Preparation and evaluation of thin-film sodium tungsten bronzes/ Harold E. Kautz [et al.]
NASA TM X-2986 – Mass transfer in a 1370 [degree] C (2500 [degree] F) lithium thermal-convection loop/ Coulson M. Scheuermann
NASA TM X-2992 – Terminal-shock and restart control of a mach 2.5, axisymmetric, mixed-compression inlet with 40-percent internal contraction/ Robert J. Baumbick, Robert E. Wallhagen and Robert C. Seidel
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