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NASA technical note

データ種別 図書
出版者 Washington D.C. : National Aeronautics and Space Administration ; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield,
本文言語 英語

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1 D-75 Factors Affecting the Plasticity of Sodium Chloride, Lithium Fluoride, and Magnesium Oxide Single Crystals / Stearns, Carl A., Pack, Ann E., Lad, Robert A. Washington, D.C. (USA) : National Aeronautics and Space Administration , 1959.10
2 D-195 Evolution of amplified waves leading to transition in a boundary layer with zero pressure gradient / Klebanoff, P.S., Tidstrom, K.D. Washington, DC (USA) : National Aeronautics and Space Administration , 1959.9
3 D-329 RADIATION SHIELDING OF THE STAGNATION REGION BY TRANSPIRATION OF AN OPAQUE GAS / HOWE, JOHN THOMAS(NASA AMES RESEARCH CENTER) : National Aeronautics and Space Administration , 1960
4 D-875 Heat transfer to an electrically conducting fluid flowing in a channel with a transverse magnetic field / Morris Perlmutter, Robert Siegel Cleveland, OH (USA) : National Aeronautics and Space Administration. Lewis Research Center , 1961.8
5 D-891 Laminar Heat-Transfer and Pressure-Distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium / Richard D. Wagner Jr., W. Clint Pine, Arthur Henderson Jr. : National Aeronautics and Space Administration , 1961.6
6 D-893 PRESSURE LOADS PRODUCED ON A FLAT-PLATE WING BY ROCKET JETS EXHAUSTING IN A SPANWISE DIRECTION BELOW THE WING AND / FALANGA, RALPH A.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
7 D-904 INVESTIGATION OF THE NATURAL FREQUENCIES AND MODE SHAPES OF LIQUIDS IN OBLATE SPHEROIDAL TANKS / LEONARD, H. WAYNE (NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
8 D-907 LOCAL AERODYNAMIC HEAT TRANSFER AND BOUNDARY-LAYER TRANSITION ON ROUGHENED SPHERE-ELLIPSOID BODIES AT MACH NUMBER / DEVEIKIS, WILLIAM D.(NASA LANGLEY RESEACRH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
9 D-910 MAGNETIC IGNLTION OF PULSED GAS DISCHARGES IN AIR OF LOW PRESSURE IN A COAXIAL PLASMA GUN / THOM, KARLHEINZ(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration , 1961
10 D-932 BOUNDARY-LAYER TRANSITION ON A GROUP OF BLUNT NOSE SHAPES AT A MACH NUMBER OF 2.20 / JACKSON, MARY W.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration , 1961
11 D-944 CONFIGURATION FACTORS FOR EXCHANGE OF RADIANT ENERGY BETWEEN AXISYMMETRICAL SECTIONS OF CYLINDERS, CONES, AND / BUSCHMAN, ALBERT J., JR.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration , 1961
12 D-955 HEAT TRANSFER AND BOUNDARY-LAYER TRANSITION ON A HIGHLY POLISHED HEMISPHERE-CONE IN FREE FLIGHT AT MACH NUMBERS UP TO / BUGLIA, JAMES J.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
13 D-959 MEASUREMENT OF FLOW ANGULARITY AT SUPERSONIC AND HYPERSONIC SPEEDS WITH THE USE OF A CONICAL PROBE / SWALLEY, FRANK E.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
14 D-960 EFFECTS OF CHANGING STRESS AMPLITUDE ON THE RATE OF FATIGUE-CRACK PROPAGATION IN TWO ALUMINUM ALLOYS / HUDSON, C. MICHAEL(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration , 1961
15 D-962 LAMINAR HEAT-TRANSFER AND PRESSURE MEASUREMENTS AT A MACH NUMBER OF 6 ON SHARP AND BLUNT 15 DEG HALF-ANGLE CONES AT / CONTI, RAUL J.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
16 D-967 MEASUREMENT AND EMPIRICAL CORRELATION OF TRANSPIRATION-COOLING PARAMETERS ON A 25 DEGREE CONE IN A TURBULENT / WALTON, THOMAS E., JR.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
17 D-988 FREE-FLIGHT INVESTIGATION OF HEAT TRANSFER TO AN UNSWEPT CYLINDER SUBJECTED TO AN INCIDENT SHOCK AND FLOW / CARTER, HOWARD S.(NASA LANGLEY RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
18 D-1054 A Technique for Increasing the Sensitivity of a Solid-State Fission Probe / Steinberg, Robert Washington, D.C. (USA) : National Aeronautics and Space Administration , 1961.8
19 D-1072 HEAT TRANSFER AT THE REATTACHMENT ZONE OF SEPARATED LAMINAR BOUNDARY LAYERS / CHUNG, PAUL M.(NASA AMES RESEARCH CENTER) : National Aeronautics and Space Administration , 1961
20 D-1088 RADIANT HEAT TRANSFER BETWEEN NONGRAY PARALLEL PLATES OF TUNGSTEN / BRANSTETTER, J. ROBERT(NASA LEWIS RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
21 D-1095 INTERACTION OF HIGHLY UNDEREXPANDED JETS WITH SIMULATED LUNAR SURFACES / STITT, LEONARD E.(NASA LEWIS RESEARCH CENTER) : National Aeronautics and Space Administration(National Aeronautics and Space Administration) , 1961
22 D-3665 RELAY IRADIATION EFFECTS EXPERIMENT. / WADDEL, R.C. : National Aeronautics and Space Administration
23 D-3772 EXTRUSION OF 1/2- AND 3/8-INCH-DIAMETER, THIN-WALL TUNGSTEN TUBING USING THE FLOATING-MANDREL TECHNIQUE. / BLANKENSHIP,C.P. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
24 D-4000 GENERALIZED POTENTIALS FOR INELASTIC SCATTERING. / VOLKIN,H.C. : National Aeronautics and Space Administration
25 D-4305 EXCITED STATES OF XENON 128. / JULIAN,G.M. Washington, D.C. : National Aeronautics and Space Administration
26 D-4472 PERIODIC, SMALL-AMPLITUDE SOLUTIONS TO THE SPATIALLY UNIFORM PLASMA CONTINUITY EQUATIONS. / ROTH,J.R. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
27 D-4651 DYNAMICS OF A ONE-DIMENSIONAL PLASMA SHEATH. / HOHL,F. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
28 D-4708 The preheating of plasma in a megajoule theta-pinch experiment / Cilliers, W.A., Norwood, J. Jr., Oertel, G.K. Washington, D.C. (USA) : National Aeronautics and Space Administration , 1968.9
29 D-4758 ANOMALOUS DIFFUSION IN A PLASMA FORMED FORM THE EXHAUST BEAM OF AN ELECTRON-BOMBARDMENT ION THRUSTER. / COHEN,A.J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
30 D-4923 EFFECTS OF REACTOR RADIATION ON 22-VOLT SILICON VOLTAGE REGULATOR DIODES. / WEINSTEIN, S.T. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
31 D-4932 ELASTIC SCATTERING OF 21 MEV PROTONS FROM NITROGEN 14, OXYGEN 16, ARGON 40, NICKEL 58, AND TIN 116. / REGIS,N.B. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
32 D-5066 HARTREE-FOCK CALCULATIONS WITH WOOD-SAXON BASIS FUNCTIONS. / FORD,W.F. : National Aeronautics and Space Administration
33 D-5215 NEW MOMENTUM INTEGRAL METHOD FOR TREATING MAGNETOHYDRODYNAMIC AND SIMPLE HYDRODYNAMIC ENTRANCE FLOWS. / SCHWIRIAN, R.E. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
34 D-5332 MAGNETOSPHERIC DUCT PROPAGATION RESEARCH USIGN ALOUETTE-2 TOPSIDE-SOUNDER OBSERVATIONS. / RAMASASTRY,J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
35 D-5348 MECHANICAL PROPERTIES OF ARC-MELTED TUNGSTEN-RHENIUM-HAFNIUM-CARBON ALLOYS. / KLOPP,W.D. : National Aeronautics and Space Administration
36 D-5355 DYNAMIC STRAIN AGING IN CARBIDE STRENGTHENED MOLYBDENUM ALLOYS. / RAFFO,P.L. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
37 D-5396 SPECTROSCOPIC STUDY OF A HELIUM ARC. / SCHERRER,V.E. : National Aeronautics and Space Administration
38 D-5407 COMPUTER PLOTTING DESCRIPTION OF ION-MOLECULE COLLISIONS WITH LONG-LIVED CAPTURE COMPLEXES. / DUGAN, J.V. : National Aeronautics and Space Administration
39 D-5751 STUDY OF BRAYTON CYCLE POWER GENERATION SYSTEM USING SNAP-8 NUCLEAR REACTOR AS AN ENERGY SOURCE. / GUENTERT,D.C. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
40 D-5836 PERFORMANCE AND DIAGNOSTICS OF A WATER-COOLED MAGNETOPLASMADYNAMIC ARC THRUSTER. / CONNOLLY,D.J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
41 D-5905 ISOTOPE EFFECT IN BETA-ZIRCONIUM. / GRAHAM, D. : National Aeronautics and Space Administration
42 D-6044 LONG TIME CREEP BEHAVIOR OF TANTALUM 10-TUNGSTEN IN HIGH VACUUM. / TITRAN,R.H. Washington, D.C. : National Aeronautics and Space Administration
43 D-6047 EXPERIMENTAL INVESTIGATION OF SINGLE PARTICLE BEHAVIOR IN AN AXISYMMETRIC MAGNETIC FIELD. / SCHERTLER,R.J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
44 D-6079 ELECTRON PARAMAGNETIC RESONANCE STUSY OF CHROMIUM (+3) IN X-RAY IRRADIATED RUBY. / LIU,D.C. : National Aeronautics and Space Administration
45 D-6284 GENERAL FORMULA FOR THE DECAY LIFETIMES OF THE STARFISH ELECTRONS. / STASSINOPOULOS,E.G. : National Aeronautics and Space Administration
46 D-6308 MECHANICAL PROPERTIES OF A TUNGSTEN 23.4-PERCENT-RHENIUM 0.27-PERCENT-HAFNIUM CARBON ALLOY. / KLOPP,W.D. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
47 D-6330 EFFECTS OF NUCLEAR RADIATION ON A HIGH RELIABILITY SILICON POWER DIODE 3: JUNCTION CAPACITANCE. / BEEN,J.F. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
48 D-6358 RADIATION-INDUCED PREPARATION OF ANTIMONY FROM SOLUTIONS OF ANTIMONY (III) CHLORIDE IN ORGANIC LIQUIDS. / PHILIPP,W.H. : National Aeronautics and Space Administration
49 D-6390 DEVELOPMENT OF COLUMBIUM ALLOY WC3015. / TAVASSOLI,A.A. Washington, D.C. : National Aeronautics and Space Administration
50 D-6464 ENERGY DEPENDENCE OF ELECTRON INDUCED RADIATION DAMAGE IN TUNGSTEN. / DICARLO,J.A. Washington, D.C. : National Aeronautics and Space Administration
51 D-6494 FAST NEUTRON REACTIVITY EFFECTS FOR REFRACTORY METALLIC SAMPLES MEASURED IN A THERMAL HOMOGENEOUS REACTOR. / PIERCE,C.R. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
52 D-6600 ESTIMATION OF GALACTIC COSMIC RAY PENETRATION AND DOSE RATES / BURRELL, M.O. Washington, D.C. : National Aeronautics and Space Administration
53 D-6687 ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF THE COAXIAL PLASMA GUN FOR USE AS A PARTICLE ACCELERATOR. / SHRIVER,E.L. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
54 D-6699 DESIGN, PERFORMANCE, AND EVALUATION OF A DIRECT CURRENT CONTACTOR FOR SPACE NUCLEAR ELECTRICAL SYSTEMS / MUELLER,L.A. : National Aeronautics and Space Administration
55 D-6704 ELECTROTHERMAL OSCILLATIONS AND THE QUASILINEAR THEORY OF ELECTRON ENTHALPY FLUCTUATIONS IN MAGNETOHYDRODYNAMIC GENERATO / SMITH,J.M. : National Aeronautics and Space Administration
56 D-6742 PARTIAL REFLECTIONS OF RADIO WAVES FROM THE LOWER IONOSPHERE / CONNOLLY,D.J. : National Aeronautics and Space Administration
57 D-6758 EFFECTS OF SIMULATED SPACE RADIATION ON SELECTED OPTICAL MATERIALS / NICOLETTA,C.A. : National Aeronautics and Space Administration
58 D-6834 SHORT-RANGE CORRELATIONS IN CARBON-12, OXYGEN-16, AND NEON-20 INTRISIC PROPERTIES / BRALEY,R.C. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
59 D-6840 OPTICAL ABSORPTION IN FUSED SILICA AT ELEVATED TEMPERATURES DURING 15 MEV ELECTRON IRRADIATION / SMITH,A.B. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
60 D-6878 CRITICALITY EXPERIMENTS AND ANALYSIS OF MOLYBDENUM REFLECTED CYLINDRICAL URANYL FLUORIDE WATER SOLUTION REACTORS. / FIENO,D. : National Aeronautics and Space Administration
61 D-7000 ALLOY SOFTENING IN GROUP VIA METALS ALLOYED WITH RHENIUM. / STEPHEN,J.R. : National Aeronautics and Space Administration
62 D-7025 ELECTRON RADIATION EFFECTS IN RUBY. / GRIMES,H.H. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
63 D-7219 HEAT PIPE INVESTIGATIONS / MARSHBURN,J.P. Washington, D.C. : National Aeronautics and Space Administration
64 D-7353 Characteristics and performance of a superconducting bumpy-torus magnet facility for plasma research / Roth, J.R. [et al.] Washington, D.C. (USA) : National Aeronautics and Space Administration , 1973.8
65 D-7413 TRAPPING OF HYDROGEN ATOMS IN X-IRRADIATED SALTS AT ROOM TEMPERATURE AND THE DECAY KINETICS / MAY,C.E. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
66 D-7534 LIGHT BULB HEAT EXCHANGER FOR MAGNETOHYDRODYNAMIC GENERATOR APPLICATIONS PRELIMINARY EVALUATION / SMITH,J.M. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
67 D-7536 INTERLABORATORY COMPARISON OF CHEMICAL ANALYSIS OF URANIUM MONONITRIDE / MERKLE,E.J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
68 D-7540 EFFECT OF OUTDOOR EXPOSURE AT AMBIENT AND ELEVATED TEMPERATURES ON FATIGUE LIFE OF TI6AL4V TITANIUM ALLOY SHEET IN THE A / PHILLIPS,F.P. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
69 D-7548 EFFECT OF LONG TIME ELEVATED TEMPERATURE EXPOSURES TO VACUUM AND LITHIUM ON THE PROPERTIES OF A TANTALUM ALLOY T 111 / BUZZARD,R.J. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
70 D-7561 COLLISIONLESS RELAXATION IN SPIRAL GALAXY MODELS / HOHL,F. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
71 D-7765 ION HEATING IN A PLASMA FOCUS / HOHL,F. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
72 D-7773 STRESS-RUPTURE STRENGTH AND MICROSTRUCTURAL STABILITY OF TUNGSTEN-HAFNIUM-CARBON-WIRE REINFORCED SUPERALLOY COMPOSITES / PETRASEK,D.W. : National Aeronautics and Space Administration
73 D-7838 EFFECTS OF ALLOY COMPOSITION IN ALLEVIATING EMBRITTLEMENT PROBLEMS ASSOCIATED WITH THE TANTALUM ALLOY T-111 / STEPHENS,J.R. : National Aeronautics and Space Administration
74 D-7847 HARDNESS BEHAVIOR OF BINARY AND TERNARY NIOBIUM ALLOYS AT 77 AND 300 K / STEPHENS,J.R. : National Aeronautics and Space Administration
75 D-7854 RESULTS OF INDUCED ATMOSPHERE MEASUREMENTS FROM THE APOLLO PROGRAM / NAUMANN,R.J. : National Aeronautics and Space Administration
76 D-7858 DESIGN PERFORMANCE AND CALCULATED ERROR OF A FARADAY CUP FOR ABSOLUTE BEAM CURRENT MEASUREMENTS OF 600 MEV PROTONS / BECK,S. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
77 D-7922 GROWTH OF SURFACE AND CORNER CRACKS IN BETA-PROCESSED AND MILL-ANNEALED TI-6AL-4V / BELL,P.D. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
78 D-8095 EFFECTS OF LONG-TERM AGING ON DUCTILITY OF THE COLUMBIUM ALLOYS C-103, CB-1ZR, AND CB-752 AND THE MOLYBDENUM ALLOY MO-TZ / STEPHENS,J.R. : National Aeronautics and Space Administration
79 D-8107 NUCLEON AND HEAVY ION TOTAL AND ABSORPTION CROSS SECTION FOR SELECTED NUCLEI / WILSON,J.W. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
80 D-8112 DESIGN AND PERFORMANCE OF A NO SINGLE FAILURE CONTROL SYSTEM FOR THE MINI BRAYTON POWER CONVERSION SYSTEM / BRICHENOUGH,A.G. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
81 D-8113 EFFECTS OF CARBON AND HAFNIUM CONCENTRATIONS IN WROUGHT POWDER METALLURGY SUPERALLOYS BASED ON NASA 2B 11 ALLOY / MINER,R.V.JR. : National Aeronautics and Space Administration
82 D-8114 CHARACRTERISTICS OF THE NASA LEWIS BUMPY TORUS PLASMA GENERATED WITH POSITIVE APPLIED POTENTIALS / ROTH,J.R. : National Aeronautics and Space Administration
83 D-8115 FIXED RANGE OPTIMUM TRAJECTORIES FOR SHORT-HAUL AIRCRAFT / ERZBERGER,H. : National Aeronautics and Space Administration
84 D-8116 DENSE PLASMA FOCUS PRODUCTION IN A HYPOCYCLOIDAL PINCH / LEE,J.H. : National Aeronautics and Space Administration
85 D-8119 PROTON AND DEUTERON DOUBLE DIFFERENTIAL CROSS SECTIONS AT ANGLES FROM 10 DEG TO 60 DEG FROM BE, C, AL, FE, CU, GE, W, AN / BECK,S.M. : National Aeronautics and Space Administration
86 D-8123 EFFECT OF NATURE OF OXYGEN INTERACTIONS ON FRICTION OF TITANIUM ALUMINUM AND MOLYBDENUM / BUCKLEY,D.H. : National Aeronautics and Space Administration
87 D-8143 STUDY OF A SECTOR SPECTROPHOTOMETER AND AURORAL O (2P 2D) EMISSIONS / SWENSON, G.R. : National Aeronautics and Space Administration
88 D-8147 NOISE LIMITATIONS OF MULTIPLIER PHOTOTUBES IN THE RADIATION ENVIRONMENT OF SPACE / VIEHMANN,W. : National Aeronautics and Space Administration
89 D-8165 PRELIMINARY ASSESSMENT OF SYSTEMS FOR DERIVING LIQUID AND GASEOUS FUELS FROM WASTE OR GROWN ORGANICS / GRAHAM,R.W. : National Aeronautics and Space Administration
90 D-8185 MECHANICAL CAPACITOR. / KIRK,J.A. Washington, D.C. : National Aeronautics and Space Administration
91 D-8196 RADIONUCLIDES IN CHESAPEAKE BAY SEDIMENTS / CRESSY,P.J.JR. : National Aeronautics and Space Administration
92 D-8460 X RAY PHOTOELECTRON SPECTROSCOPIC STUDY OF SURFACE CHEMISTRY OF DIBENZYL DISULFIDE ON STEEL UNDER MILD AND SEVERE WEAR C / WHEELER,D.R. : National Aeronautics and Space Administration
93 D-8462 VOLATILIZATION OF OXIDES DURING OXIDATION OF SOME SUPERALLOYS AT 1200 C / ZAPLATYNSKY,I. : National Aeronautics and Space Administration
94 D-8464 FLOW AND HEAT TRANSFER IN A CURVED CHANNEL / BRINICH,P.F. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
95 D-8466 FACTORS AFFECTING ION KINETICS TEMPERATURE NUMBER DENSITY AND CONTAINMENT TIME IN THE NASA LEWIS BUMPY TORUS PLASMA / ROTH,J.R. : National Aeronautics and Space Administration(National Aeronautics and Space Administration)
96 D-8516 NOISE TRANSMISSION BY VISCOELASTIC SANDWICH PANELS / VAICAITIS,R. : National Aeronautics and Space Administration
97 D-8520 RANDOM AND SYSTEMATIC MEASUREMENT ERRORS IN ACOUSTIC IMPEDANCE AS DETERMINED BY THE TRANSMISSION LINE MEDTHOD : National Aeronautics and Space Administration
98 D-8525 OPTIMALITY CRITERION FOR SIZING MEMBERS OF HEATED STRUCTURES WITH TEMPERATURE CONSTRAINTS / RAO, G.V. : National Aeronautics and Space Administration
99 D-8526 IMPROVED ANALYSIS OF ELECTRON PENETRATION AND NUMERICAL PROCEDURES FOR SPACE RADIATION SHIELDING / WILSON,J.W. : National Aeronautics and Space Administration
100 D-8527 RELATION OF MORPHOLOGY OF ELECTRODEPOSITED ZINC TO ION CONCENTRATION PROFILE / MEY,C.E. : National Aeronautics and Space Administration
101 D-8528 ELASTOHYDRODYNAMIC LUBRICATION OF ELLIPTICAL CONTACTS FOR MATERIALS OF LOW ELASTIC MODULUS 1 FULLY FLOODED CONJUNCTION / HAMROCK,B.J. : National Aeronautics and Space Administration
102 D-8641 SUSCEPTIBILITY TO HOT CORROSION OF FOUR NICKEL BASE SUPERALLOYS, NASA TRW VIA, B-1900, 713C AND IN 738 / STEARNS,C.A. : National Aeronautics and Space Administration

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別書名 異なりアクセスタイトル:NASA TN
著者標目 *United States. National Aeronautics and Space Administration
書誌ID 1001413448
NCID BA12241165

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