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NASA Technical Note D-5341, October, 1969.
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Aero. Systems Div., TR-67-727, vol. III, Feb. 1962.
Powers, S.A.; Niemann, A.F., Jr.; and Der, J., Jr.:
A Numerical
Procedure for Determining the Combined Viscid-Inviscid Flow Fields
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Air Force Systems Command, AFFDL-TR-67-l24, vol. I, Dec. 1967.
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The Method of Characteristics for Three-Dimensional
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The Numerical Solution of Hyperbolic Systems of Partial
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Katskova, O.N.; and Chushkin, P.I.:
Three Dimensional Supersonic
Equilibrium Flow of a Gas Around Bodies at Angle of Attack.
NASA Technical Translation TT F-9790, 1965.
Ransom, V.H.; Thompson, H.D.; and Hoffman, J.D.:
Analysis of
Three-Dimensional Scramjet Exhaust Nozzle Flow Fields by a New Second-Order
Method of Characteristics.
AIAA Paper 69-5, presented at the Seventh
Aerospace Sciences Meeting, Jan. 20-22, 1969.
Babenko, K.I.; Voskresenskiy, G.P.; Lyubimov, A.N.; and Rusanov, V.V.:
Three-Dimensional Flow of Ideal Gas Past Smooth Bodies.
NASA Technical Translation TT F-380, 1966.
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Rakich, John V.; and Cleary, Joseph W.: Theoretical and Experimental
Study of Supersonic Steady Flow Around Inclined Bodies of Revolution.
Seventh Aerospace Sciences Meeting, Jan. 20-22, 1969, Paper 69-187.
Rakich, John V.: Numerical Calculation of Supersonic Flows of a Perfect
Gas Over Bodies of Revolution at Small Angles of Yaw.
NASA Technical Note D-2390, 1964.
Chu, Chong-Wei: Compatibility Relations and a Generalized Finite
Difference Approximation for Three-Dimensional Steady Supersonic Flow.
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McGraw-Hill Book Co., Inc., 1962.
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Properties About Blunt Bodies Moving at Supersonic Speeds in an Equilibrium
Gas.
NASA Technical Report R-204, 1964.
Briggs, Benjamin R.:
The Numerical Calculation of Flow Past Conical
Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of
Incidence.
NASA Technical Note D-340, 1960.
Moretti, G.: Inviscid Flow Field Past a Pointed Cone at an Angle of
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Rakich, John V.:
Calculation of Hypersonic Flow Over Bodies of
Revolution at Small Angles of Attack.
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NASA Technical Translation
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Gallo, William F.; and Rakich, John V.:
Investigation of Methods for
Predicting Flow in the Shock Layer Over Bodies at Small Angles of
Attack.
NASA Technical Note D-3946, 1967.
Inouye, Mamoru; Rakich, John V.; and Lomax, Harvard:
A Description of
Numerical Methods and Computer Programs for Two-Dimensional and
Axisymmetric Supersonic Flow Over Blunt-Nosed and Flared Bodies.
NASA Technical Note D-2970, 1965.
Cleary, Joseph W.:
An Experimental and Theoretical Investigation of the
Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic
Mach Numbers.
NASA Technical Note D-2969, 1965.
Cleary, Joseph W.:
Effects of Angle of Attack and Bluntness on the
Shock-Layer Properties of a 15 Degree Cone at a Mach Number of 10.6.
NASA Technical Note D-4909, 1968.
Ames Research Staff: Equations, Tables, and Charts for Compressible
Flow. NACA Report 1135, 1953.
Rakich, John V.:
Supersonic Aerodynamic Performance And Static-Stability
Characteristics Of Two Blunt-Nosed, Modified
13 Degree Half-Cone Configurations.
NASA Technical Memorandum X-375, September 1960.