Ballistic range tests of ablating and nonablating slender cones
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Engineering topics
Publications and source records attributed to Chapman, G. T..
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Aerodynamic coefficients from observed motion of body in flight, eliminating need for closed form solutions by employing numerical solutions to equations of motion
A series of balloon-borne experiments has been initiated at the Oak Ridge National Laboratory (ORNL) in cooperation with the Space Sciences Laboratory of the NASA G. C. Marshall Space Flight Center to determine the feasibility of using large (greater than 20 cc) lithium-drifted, germanium diodes to investigate the spectrum of atmospheric gamma rays (60 keV < E < 1.5 MeV) at altitudes corresponding to a few grams per cm (sup 2) residual atmosphere. The results of these measurements will also provide a basis for designing an appropriate shield for a multi-diode, highly directional gamma-ray spectrometer for use in astrophysical measurements. Two flights were accomplished during 1967 using the same two diodes and basic instrument package. Both flights were launched at the NCAR Scientific Balloon Flight Base, Palestine, Texas, and attained a float altitude of 117, 000 ft. The measured atmospheric gamma-ray spectrum shows at least one distinct line at 511 keV (annihilation radiation) superimposed on a continuous distribution of gamma rays attributable to both energy-degraded gamma rays and brems-strahlung photons. A second diode, encased in a passive shield of plastic and lead, shows the expected lines resulting from both neutron inelastic scattering and capture in the germanium. Data acquisition was accomplished on an event-by-event basis through the use of 512-channel, on-board ADC and word-generator circuits and a ground-based, on-line telemetry decoder. The decoder makes it possible to store the data in the memory of a modified pulse-height analyzer simultaneously with storage on magnetic tape. This provides a real-time visual observation of the data as it is accumulated and greatly facilitates preflight calibrations.
Computer program for analyzing free flight motions of axisymmetric bodies to determine aerodynamic coefficients
Gamma rays from bombardment by protons and alpha particles, discussing production cross sections in carbon and oxygen obtained from absolute spectra
Orderly three dimensional processes in turbulent boundary layers on biconic, concave, and convex ablating bodies in Mach 7 airstream
Flow model for three dimensional processes in turbulent boundary layers of ablating hypersonic Plexiglas bodies
Contribution of secondary gamma rays to radiation dosage produced by charged particles in space
Heat transfer in stagnation-point laminar boundary layer with mass injection and absorption of incident radiation
Total boundary layer mass flow with mass transfer at wall
Static and dynamic stability and drag of blunt- nosed flare-stabilized bodies at velocities up to 8.2 km per second
Mathematical models for reducing errors and analyzing aerodynamic force and moment data from ballistics tests
Near zero lift drag coefficient relationship to initial slope of normal force coefficient curve obtained from Newtonian theory
Aerodynamic characteristics of short axisymmetric bodies at Mach numbers 5 to 15
Static and dynamic stability and drag of blunt- nosed flare-stabilized bodies at velocities up to 8.2 kilometers per second
Factors degrading dynamic stability results from ballistic range flight tests
Laminar convective heat transfer and boundary layer equations for cones at escape velocity