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
|