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NASA Technical Reports List
Number
|
Title
|
Author(s)
|
Date
|
Pages
|
R-1
|
Supersonic Flow Past a Family of Blunt Axisymmetric
Bodies
|
Milton D. Van Dyke and Helen D. Gordon
|
1959
|
25
|
R-2
|
Slender-Body Theory Based on Approximate Solution of
the Transonic Flow Equation
|
John R. Spreiter and Alberta Y. Alksne
|
1959
|
54
|
R-3
|
Nearly Circular Transfer Trajectories for Descending
Satellites
|
George M. Low
|
1959
|
17
|
R-4
|
Stability of a Horizontal Fluid Layer With Unsteady
Heating From Below and Time-Dependent Body Force
|
Arthur W. Goldstein
|
1959
|
15
|
R-5
|
Application of Morse Potential Function to Cubic
Metals
|
Louis A. Girifalco and Victor G. Weizer
|
1959
|
14
|
R-6
|
Experimental and Theoretical Studies of Axisymmetric
Free Jets
|
Eugene S. Love, Carl E. Grigsby, Louise P. Lee, and
Mildred J. Woodling
|
1959
|
292
|
R-7
|
Turbulent Boundary Layer on a Yawed Cone in a
Supersonic Stream
|
Willis H. Braun
|
1959
|
16
|
R-8
|
Mass Transfer Cooling Near the Stagnation Point
|
Leonard Roberts
|
1959
|
16
|
R-9
|
A Theoretical Study of Stagnation-Point Ablation
|
Leonard Roberts
|
1959
|
11
|
R-10
|
Stagnation-Point Shielding by Melting and
Vaporization
|
Leonard Roberts
|
1959
|
24
|
R-11
|
An Approximate Analytical Method for Studying Entry
Into Planetary Atmospheres
|
Dean R. Chapman
|
1959
|
44
|
R-12
|
Effect of the Proximity of the Wing First-Bending
Frequency on the Airplane Dynamic-Response Factor
|
Carl R. Huss and James J. Donegan
|
1959
|
20
|
R-13
|
Effect of a Stringer on the Stress Concentration Due
to a Crack in a Thin Sheet
|
J. Lyell Sanders,
Jr.
|
1959
|
10
|
R-14
|
A Method for Calculation of Hydrodynamic Lift for
Submerged and Planing Rectangular Lifting Surfaces
|
Kenneth L. Wadlin and Kenneth W. Christopher
|
1959
|
13
|
R-15
|
Approximate Analytical Solutions for Hypersonic Flow
Over Slender Power Law Bodies
|
Harold Mirels
|
1959
|
24
|
R-16
|
Effects of Mach Number and Wall-Temperature Ratio on
Turbulent Heat Transfer at Mach Numbers From 3 to 5
|
Thorval Tendeland
|
1959
|
15
|
R-17
|
Analysis of Turbulent Flow and Heat Transfer on a
Flat Plate at High Mach Numbers With Variable Fluid
Properties
|
R. G. Deissler and A. L. Loeffler, Jr.
|
1959
|
33
|
R-18
|
Several Methods for Aerodynamic Reduction of
Static-Pressure Sensing Errors for Aircraft at Subsonic,
Near-sonic, and Low Supersonic Speeds
|
Virgil S. Ritchie
|
1959
|
23
|
R-19
|
Theoretical Analysis of the Longitudinal Behavior of
an Automatically Controlled Supersonic Interceptor
During the Attack Phase
|
Ordway B. Gates, Jr., and C. H. Woodling
|
1959
|
22
|
R-20
|
Tire-to-Surface Friction-Coefficient Measurements
With a C-123B Airplane on Various Runway Surfaces
|
Richard H. Sawyer and Joseph J. Kolnick
|
1959
|
32
|
R-21
|
On Solutions for the Transient Response of Beams
|
Robert W. Leonard
|
1959
|
33
|
R-22
|
Boundary-Layer Displacement Effects in Air at Mach
Numbers of 6.8 and 9.6
|
Mitchel H. Bertram
|
1959
|
32
|
R-23
|
Effect of Surface Roughness on Characteristics of
Spherical Shock Waves
|
Paul W. Huber and Donald R. McFarland
|
1959
|
25
|
R-24
|
An Improved First-Approximation Theory for Thin
Shells
|
J. Lyell Sanders,
Jr.
|
1959
|
11
|
R-25
|
Boundary-Induced Downwash Due to Lift in a
Two-Dimensional Slotted Wind Tunnel
|
S. Katzoff and Raymond L. Barger
|
1959
|
19
|
R-26
|
Skin-Friction Measurements in Incompressible Flow
|
Donald W. Smith and John H. Walker
|
1959
|
35
|
R-27
|
Theoretical and Experimental Investigation of Heat
Conduction in Air, Including Effects of Oxygen
Dissociation
|
C. Frederick Hansen, Richard A. Earlky, Frederick E.
Alzofon, and Fred C. Witteborn
|
1959
|
25
|
R-28
|
Practical Solution of Plastic Deformation Problems
in Elastic-Plastic Range
|
A. Mendelson
and S. S. Manson
|
1959
|
24
|
R-29
|
Effect of Flow Incidence and Reynolds Number on
Low-Speed
Aerodynamic Characteristics of Several Noncircular
Cylinders with Applications to Directional Stability and
Spinning
|
Edward C. Polhamus
|
1959
|
25
|
R-30
|
Local Instability of the Elements of A Truss-Core
Sandwich Plate
|
Melvin S. Anderson
|
1959
|
13
|
R-31
|
Analysis of Turbulent Flow and Heat Transfer in
Noncircular Passages
|
Robert G. Deissler and Maynard F. Faylor
|
1959
|
18
|
R-32
|
Tables of the Bessel-Kelvin Functions ber, Bei, Ker,
Kei, and Their Derivatives for the Argument Range
0(0.01)107.50
|
Herman H. Lowell
|
1959
|
291
|
R-33
|
Design of Axisymmetric Exhaust Nozzles by Method of
Characteristics Incorporating a Variable Isentropic
Exponent
|
Eleanor Costilow Guentert and Harvey E. Neumann
|
1959
|
17
|
R-34
|
On Fully Developed Channel Flows:
Some Solutions and Limitations, and Effects of
Compressibility, Variable Properties, and Body Forces
|
Stephen H. Maslen
|
1959
|
22
|
R-35
|
Ground Reflection of Jet Noise
|
Walton L. Howes
|
1959
|
29
|
R-36
|
Two-Dimensional Diffusion Theory Analysis of
Reactivity Effects of a Fuel-Plate-Removal Experiment
|
Edward R. Gotsky, James P. Cusick, and Donald Bogart
|
1959
|
15
|
R-37
|
Boundary-Layer Stability Diagrams for Electrically
Conducting Fluids in the Presence of a Magnetic Field
|
Vernon J. Rossow
|
1959
|
16
|
R-38
|
The Theory of Diffusion in Strained Systems
|
Louis A. Girifalco and Hubert H. Grimes
|
1959
|
20
|
R-39
|
The Phenomenon of Change in Buckle Pattern in
Elastic Structures
|
Manuel Stein
|
1959
|
9
|
R-40
|
Loads and Deformations of Buckled Rectangular Plates
|
Manuel Stein
|
1959
|
27
|
R-41
|
Normal Component of Induced Velocity for Entire
Field of a Uniformly Loaded Lifting Rotor with Highly
Swept Wake as Determined by Electromagnetic Analog
|
Walter Castles, Jr., Howard L. Durham, Jr., and
Jirair Kevorkian
|
1959
|
23
|
R-42
|
Similar Solutions for the Compressible Boundary
Layer on a Yawed Cylinder With Transpiration Cooling
|
Ivan E. Beckwith
|
1959
|
37
|
R-43
|
Analysis of Injection-Velocity Effects on Rocket
Motor Dynamics and Stability
|
Herbert G. Hurrell
|
1959
|
26
|
R-44
|
A Phenomenological Theory for the
|
Elbridge Z. Stowell
|
1959
|
15
|
R-45
|
Effect of Body Perturbations on Hypersonic Flow Over
Slender Power Law Bodies
|
Harold Mirels and Philip R. Thornton
|
1959
|
30
|
R-46
|
Pressure and Force Characteristics of Noncircular
Cylinders as Affected By Reynolds Number With a Method
Included for Determining the Potential Flow About
Arbitrary Shapes
|
Edward C. Polhamus, Edward W. Geller, and Kalman J.
Grunwald
|
1959
|
42
|
R-47
|
Second-Order Slender-Body Theory—Axisymmetric Flow
|
Milton D. Van Dyke
|
1959
|
26
|
R-48
|
A Systematic Kernel Function Procedure for
Determining Aerodynamic Forces on Oscillating or Steady
Finite Wings at Subsonic Speeds
|
Charles E. Watkins, Donald S. Woolston, and Herbert
J. Cunningham
|
1959
|
21
|
R-49
|
Summary and Analysis of Horizontal-Tail Contribution
to Longitudinal Stability of Swept-Wing Airplanes at Low
Speeds
|
Robert H. Neely and Roland F. Griner
|
1959
|
87
|
R-50
|
Approximations for the Thermodynamic and Transport
Properties of High-Temperature Air
|
C. Frederick Hansen
|
1959
|
35
|
R-51
|
Adsorption of Halogenated Fire-Extinguishing Agents
on Powders
|
Allen J. Barduhn, Bhailal S. Patel, Walter Meye and
Bronislaw B. Smura
|
1960
|
41
|
R-52
|
Similarity of Far Noise Fields of Jets
|
Walton L. Howes
|
1960
|
44
|
R-53
|
Trajectories With Constant Tangential Thrust in
Central Gravitational Fields
|
W. E. Moeckel
|
1960
|
73
|
R-54
|
Factors That Affect Operational Reliability of
Turbojet Engines
|
Lewis Center Staff
|
1960
|
211
|
R-55
|
An Analysis of the Corridor and Guidance
Requirements for Supercircular Entry Into Planetary
Atmospheres
|
Dean R. Chapman
|
1960
|
47
|
R-56
|
Graphical Presentation of Difference Solutions for
Transient Radial Heat Conduction in Hollow Cylinders
With Heat Transfer at the Inner Radius and Finite Slabs
With Heat Transfer at One Boundary
|
James E. Hatch, Ralph L. Schacht, Lynn U. Albers,
and Paul G. Saper
|
1960
|
49
|
R-57
|
Status of Spin Research for Recent Airplane Designs
|
Anshal I. Neihouse, Walter J. Klinar, and Stanley H.
Scher
|
1960
|
54
|
R-58
|
Calculation of Aerodynamic Loading and Twist
Characteristics of a Flexible Wing at Mach Numbers
Approaching 1.0 and Comparison With Experiment
|
John P. Mugler, Jr.
|
1960
|
17
|
R-59
|
Predicted Behavior of Rapidly Heated Metals in
Compression
|
Elbridge Z. Stowell and George J. Heimerl
|
1960
|
7
|
R-60
|
A Study of Some Factors Affecting Rolling-Contact
Fatigue Life
|
Thomas L. Carter
|
1960
|
48
|
R-61
|
Stall Propagation in a Cascade of Airfoils
|
Anthony R. Kriebel, Barry S. Seidel, and Richard G.
Schwind
|
1960
|
51
|
R-62
|
An Analysis of Ablation-Shield Requirements for
Manned Reentry Vehicles
|
Leonard Roberts
|
1960
|
58
|
R-66
|
A Study of the Asymmetric Transonic Flow Past a
Sharp Leading Edge
|
Howard A. Stine, Cleo B. Wagoner, and Alvin L. Lugn,
Jr.
|
1960
|
70
|
R-67
|
Propellant Vaporization as a Design Criterion for
Rocket-Engine Combustion Chambers
|
Richard J. Priem and Marcus F. Heidmann
|
1960
|
127
|
R-68
|
The Interactions Between Nitrogen and Oxygen
Molecules
|
Willard E. Meador, Jr.
|
1960
|
25
|
R-69
|
Calculated Responses of a Large Sweptwing Airplane
to Continuous Turbulence with Flight-Test Comparisons
|
Floyd V. Bennett and Kermit G. Pratt
|
1960
|
25
|
R-70
|
An Evaluation of Effects of Flexibility on Wing
Strains in Rough Air for a Large Swept-Wing Airplane by
Means of Experimentally Determined Frequency-Response
Functions with an Assessment of Random-Process
Techniques Employed
|
Thomas L. Coleman, Harry Press, and May T. Meadows
|
1960
|
33
|
R-71
|
Jet-Boundary Corrections for Lifting Rotors Centered
in Rectangular Wind Tunnels
|
Harry H. Heyson
|
1960
|
62
|
R-72
|
A Supersonic Area Rule and an Application to the
Design of a Wing-Body Combination With High Lift-Drag
Ratios
|
Richard T. Whitcomb and John R. Sevier, Jr.
|
1960
|
14
|
R-73
|
A Study of the Simulation of Flow With Free-Stream
Mach Number 1 in a Choked Wind Tunnel
|
John R. Spreiter, Donald W. Smith, and B. Jeanne
Hyett
|
1960
|
36
|
R-74
|
The Lateral Response of Airplanes to Random
Atmospheric Turbulence
|
John M. Eggleston and William H. Phillips
|
1960
|
59
|
R-152
|
The Aerodynamic Design of Wings With Cambered Span
Having Minimum Induced Drag
|
Clarence D. Cone, Jr.
|
1963
|
63
|
R-154
|
Radiant Heat Transfer to Absorbing Gases Enclosed
Between Parallel Flat Plates With Flow and Conduction
|
Thomas H. Einstein
|
1963
|
23
|
R-155
|
Spin Dynamics of Manned Space Stations
|
Peter R. Kurzhals and Claude R. Keckler
|
1963
|
58
|
R-156
|
Radiant Heat Transfer to Absorbing Gases Enclosed in
a Circular Pipe With Conduction, Gas Flow, and Internal
Heat Generation
|
Thomas H. Einstein
|
1963
|
26
|
R-157
|
Radiative Heat Transfer Between Planar Surfaces With
Filleted Junctures
|
Wm. Prichard Jones
|
1963
|
22
|
R-158
|
Tables for Eccentric and True Anomaly in Elliptic
Orbits
|
Jack T. Kent, George B. Taack, Jr., and David C.
Larson
|
1963
|
206
|
R-159
|
Solutions of the Ionized Radiating Shock Layer,
Including Reabsorption and foreign Species Effects, and
Stagnation Region Heat Transfer
|
John T. Howe and John R. Viegas
|
1963
|
21
|
R-160
|
Considerations of the Motion of a Small Body in the
Vicinity of the Stable Libration Points of the
Earth-Moon System
|
William H. Michael, Jr.
|
1963
|
24
|
R-161
|
Theoretical and Experimental Study of the
Interaction of Free-Surface Waves on Liquid Metals With
Transverse Magnetic Fields (One-Dimensional Unsteady
Waves)
|
Vernon J. Rossow
|
1963
|
111
|
R-162
|
A Theory of Space-Probe Entry Under Conditions of
High Mass Loss
|
Frederick C. Grant
|
1963
|
18
|
R-163
|
Hypersonic Shock-Heated Flow Parameters for
Velocities to 46,000 Feet per Second and Altitudes to
323,000 Feet
|
Paul W. Huber
|
1963
|
74
|
R-164
|
Theoretical Studies of Supersonic Two-Dimensional
and Axisymmetric Nonequilibrium Flow, Including
Calculations of Flow Through a Nozzle
|
James J. Der
|
1963
|
48
|
R-165
|
Wall-Pressure Fluctuations and Pressure-Velocity
Correlations in a Turbulent Boundary Layer
|
John S. Serafini
|
1963
|
78
|
R-166
|
Elastic Constants for Bending and Twisting of
Corrugation-Stiffened Panels
|
W. Jefferson Stroud
|
1963
|
42
|
R-167
|
Charts for the Analysis of Isentropic
One-Dimensional Unsteady Expansions in Equilibrium Real
Air With Particular Reference to Shock-Initiated Flows
|
William L. Grose and Robert L. Trimpi
|
1963
|
17
|
R-168
|
Directional Dependence of Counting Rates From
Explorer IV (Satellite 1958 Epsilon)
|
Robert Jordan Naumann
|
1963
|
73
|
R-169
|
Solar Proton Manual
|
Edited by Frank B. McDonald, contributed by C. E.
Fichtel, D. E. Guss, H. H. Malitson, K.G. McCracken, K.
W. Ogilvie, and W. R. Webber
|
1963
|
117
|
R-170
|
Axial and Radial Magnetic Fields of Thick,
Finite-Length Solenoids
|
Gerald V. Brown, Lawrence Flax, Eugene C. Itean, and
James C. Laurence
|
1963
|
98
|
R-171
|
The Correlation of Oblique Shock Parameters for
Ratios of Specific Heats from 1to 5/3 With Application
to Real Gas Flows
|
Mitchel H. Bertram and Barbara S. Cook
|
1963
|
70
|
R-172
|
Generalized Treatment of Plane Electromagnetic Waves
Passing Through an Isotropic Inhomogeneous Plasma Slab
at Arbitrary Angles of Incidence
|
Calvin T. Swift and John S. Evans
|
1963
|
41
|
R-173
|
The Structure and Strength of the Inner Planets
|
Gordon J. F. MacDonald Goddard Space Flight Center
Greenbelt, Maryland
|
1963
|
84
|
R-174
|
Theoretical Performance of Electrostatic Thrustors
With Analytic Space-Charge Flows
|
William R. Mickelsen
|
1963
|
202
|
R-176
|
A Discussion of Halphen’s Method for Secular
Perturbations and Its Application to the Determination
of Long Range Effects in the Motions of Celestial
Bodies. Part 1.
|
Peter Musen
|
1963
|
52
|
R-179
|
Determination and Analysis of Numerical Smoothing
Weights
|
Ronald J. Graham
|
1963
|
28
|
R-182
|
Reynolds Number Effects on the Induced Pressures of
Cylindrical Bodies With Different Nose Shapes and Nose
Drag Coefficients in Helium at a Mach Number of 24
|
Richard D. Wagner, Jr., and Ralph Watson
|
1963
|
1
|
R-185
|
Aerodynamic Heating of Conical Entry Vehicles at
Speeds in Excess of Earth Parabolic Speed
|
H. Julian Allen, Alvin Seiff, and Warren Winovich
|
1963
|
1
|
R-186
|
On the Mechanism of Ductile Bending in Ionic
Crystals
|
Charles E. May
|
1963
|
15
|
R-206
|
On the Stability of the Boundary of the Geomagnetic
Field
|
John R. Spreiter and Audrey L. Summers
|
1965
|
30
|
R-212
|
Theoretical Analysis of Several Linear Steady-Flow
Plasma Accelerators With Crossed Electric and Magnetic
Fields
|
Clarence W. Matthews
|
1964
|
51
|
R-213
|
Correlation of Sonic-Boom Theory With Wind-Tunnel
and Flight Measurements
|
Harry W. Carlson
|
1964
|
25
|
R-214
|
A Spectrographic Analysis of a 1-Foot
Hypersonic-Arc-Tunnel Airstream Using an Electron Beam
Probe
|
Daniel I. Sebacher and Roy J. Duckett
|
1964
|
18
|
R-215
|
Radiative Transfer in a Cloudy Atmosphere
|
R. E. Samuelson
|
1965
|
87
|
R-217
|
Liouville’s Equation and the N-Body Problem
|
R. G. Langebartel
|
1965
|
56
|
R-218
|
Polarization of Protons from (d,p) Reactions at 21
MEV
|
Edmund T. Boschitz and John S. Vincent
|
1964
|
18
|
R-219
|
Characteristics of a Continuous-Flow Induction
Plasma Accelerator
|
J. D. Brooks, W. D. Beasley, and R. L. Barger
|
1965
|
27
|
R-220
|
Analysis of Heat-Transfer Effects in Rocket Nozzles
Operating With Very High-Temperature Hydrogen
|
John R. Howell, Mary K. Strite, and Harold E. Renkel
|
1965
|
32
|
R-221
|
Analysis of Hypervelocity Perforation of a
Visco-Plastic Solid Including the Effects of
Target-Material Yield Strength
|
Robert G. Thomson
|
1965
|
39
|
R-222
|
Equations for Isentropic and Plane Shock Flows of
Mixtures of Undissociated Planetary Gases
|
Victor L. Peterson
|
1965
|
34
|
R-223
|
A Perfect-Gas Analysis of the Expansion Tunnel, a
Modification to the Expansion Tube
|
Robert L. Trimpi and Linwood B. Callis
|
1965
|
101
|
R-224
|
Convective Heat Transfer in Planetary Gases
|
Joseph G. Marvin and George S. Deiwert
|
1965
|
47
|
R-225
|
Analysis of the Errors Associated With the
Determination of Planetary Atmosphere Structure From
Measured Accelerations of an Entry Vehicle
|
Victor L. Peterson
|
1965
|
21
|
R-227
|
A Theoretical and Experimental Study of the
Nonlinear Flexural Vibrations of Thin Circular Rings
|
David A. Evensen
|
1965
|
58
|
R-228
|
Estimation of Flight Performance With Closed-Form
Approximations to the Equations of Motion
|
Charlie M. Jackson, Jr.
|
1966
|
30
|
R-229
|
Plane Thermoelastic Deformation of Internally Heated
Annular Disks or Hollow Cylinders
|
Franklyn B. Fuller
|
1966
|
43
|
R-230
|
Use of Fusible Temperature Indicators for Obtaining
Quantitative Aerodynamic Heat-Transfer Data
|
Robert A. Jones and James L. Hunt
|
1966
|
29
|
R-231
|
The Electromagnetic Torques on Spherical Earth
Satellites in a Rarefied Partially Ionized Atmosphere
|
Frank Hohl
|
1966
|
64
|
R-232
|
A Theoretical and Experimental Investigation of the
Oxidation of Molybdenum at Temperatures at Which Its
Trioxide Is Volatile
|
David R. Schryer and Gerald D. Walberg
|
1966
|
39
|
R-233
|
Syncom Engineering Report Volume I
|
Syncom Projects Office
|
1966
|
160
|
R-235
|
Investigation of the Divergence Characteristics of
Delta-Planform Canard Controls
|
A. Gerald Rainey, Perry W. Hanson, and Dennis J.
Martin
|
1966
|
32
|