Howser, Lona M.; and Tompkins, Stephen S.:
Computer Program for the Transient Response of Ablating Axisymmetric Bodies,
Including the Effects of Shape Change.
NASA Technical Memorandum X-2375, October 1971.
Tompkins, Stephen S.; Moss, James N.; Pittman, Claud M.; and Howser, Lona M.:
Numerical Analysis of the Transient Response of Ablating Axisymmetric Bodies,
Including the Effects of Shape Change.
NASA Technical Note D-6220, May 1971.
Pittman, Claud M.; and Howser, Lona M.:
Numerical Analysis of the Transient Response of an Axisymmetric Ablative Char Layer
Condigering Internal Flow Effects.
NASA Technical Note D-6895, September 1972.
Gavril, Bruce D.; and Lane, Frank:
Finite Difference Equation and Their Solution for the Transient Temperature
Distribution in Composite, Anisotropic, Generalized Bodies of Revolution.
Tech. Rep. No. 230 (Contract No. NOrd 18053), Gen. Appl. Sci. Lab., Inc., May 26, 1961.
Hovanessian, Shahen A.; and Pipes, Louis A.:
Digital Computer Methods in Engineering. McGraw-Hill Book Co., Inc., c.1969.
Peterson, W. D.; and Spanier, J.: HOT-2:
A Two-Dimensional Transient Heat Conduction Program for the CDC-6600.
WAPD-TM-669, U.S. Atomic Energy Commission, June 1967.
McClure, John A,:
TOODEE - A Two-Dimensional, Time-Dependent Heat Conduction Program.
AEC Research and Development Report IDO-17227, U.S. Atomic Energy Comm., April 1967.
Friedman, H. A.; and McFarland, B. L.:
Two-Dimensional Transient Ablation and Heat Conduction Analysis for Multimaterial Thrust Chamber Walls.
Journal of Spacecraft and Rockets, vol. 5, no. 7, July 1968, pp. 753-761.
McCuen, Peter A.; Schaefer, John W.; Lundberg, Raymond E.; and Kendall, Robert M.:
A Study of Solid-Propellant Rocket Motor Exposed Materials Behavior.
AFRPLTR-65-33, U.S. Air Force, Feb. 26, 1965.
Popper, L. A.; Toong, T. Y.; and Sutton, G. W.:
Three-Dimensional Ablation Considering Shape Changes and Internal Heat Condition.
AIAA Paper No. 70-199, Jan. 1970.
Moyer, Carl B.; Anderson, Larry W.; and Dahm, Thomas J.:
A Coupled Computer Code for the Transient Thermal Response and Ablation of
Non-Charring Heat Shields and Nose Tips.
NASA Contractor Report 1630, 1970.
Thornton, William A.; and Schmit, Lucien A., Jr.:
The Structural Synthesis of an Ablating Thermostructural Panel.
NASA Contractor Report 1215, 1968.
Swann, Robert T.; Pittman, Claud M.; and Smith, James C.:
One-Dimensional Numerical Analysis of the Transient Response of Thermal Protection Systems.
NASA Technical Note D-2976, September 1965.
Scala, Sinclaire M.; and Gilbert, Leon M.:
Sublimation of Graphite at Hypersonic Speeds.
AIAA Journal, vol. 3, no. 9, Sept. 1965, pp. 1635-1644.
McCarthy, J. F., Jr.; and Hanley, G. M.:
Earth Entry at Hyperbolic Velocities.
AIAA Paper No. 68-153, Jan. 1968.
Lees, Lester:
Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds.
Jet Propulsion, vol. 26, no. 4, Apr. 1956, pp. 259-269, 274.
Gavril, Bruce D.; and Lane, Frank:
Finite Difference Equations and Their Solution for the Transient Temperature
Distribution in Composite, Anisotropic, Generalized Bodies of Revolution.
Technical Report No. 230 (Contract No. NOrd 18053), Gen. Appl. Sci. Lab., Inc., May 26, 1961.
Brooks, William A., Jr.:
Temperature and Thermal-Stress Distributions in Some Structural Elements
Heated at a Constant Rate.
NACA Technical Note 430, August 1958.
Howell, Robert R.:
An Experimental Study of the Behavior of Spheres Ablating Under
Constant Aerodynamic Conditions.
NASA Technical Note D-1635, 1963.
Brewer, William D.: Ablative Material Performance in High Radiative Heat Flux
Environment Produced by a Carbon Dioxide Laser. AIM Paper No. 70-864,
June-July 1970.