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Flow-Field Investigation of a 0.0667-Scale Model of the X-15 Research Vehicle at Mach 4, 6, 8
Author(s): Rippey, J.
Corporate Author(s): ARO, inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-10
Report number: AEDC -TDR-201
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Tables of Thermodynamic Properties of Argon from 100 to 3000°K
Author(s): Little, Wanda J.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-04
Report number: AEDC TDR 64-68
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Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory
Author(s): Clark, E. L., Trimmer, L. L.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-03
Report number: AEDC TDR 64-25
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Theoretical Base Pressure Analysis of Axisymmetric Ejectors Without Induced Flow
Author(s): Bauer, R. C.
Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-01
Report number: AEDC TDR 64-3

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