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| Author | : General Electric Company |
| Publisher | : |
| Total Pages | : 108 |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : L.A. Marshall |
| Publisher | : |
| Total Pages | : |
| Release | : 1967 |
| Genre | : |
| ISBN | : |
| Author | : General Electric Company |
| Publisher | : |
| Total Pages | : 128 |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : General Electric Company |
| Publisher | : |
| Total Pages | : |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : General Electric Company |
| Publisher | : |
| Total Pages | : 328 |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
| Author | : O. Walchner |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1974 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
This final report summarizes the in-house research work on hypersonic stability problems, applicable to reentry dynamics. During the period 1963 to 1974 research contributions were made in the following areas: (1) Static and dynamic stability in pitch; (2) hypersonic roll damping; (3) asymmetric nose effects; (4) non linear aerodynamics; (5) stability coefficients in nonplanar motions. This in-house research effort was terminated as of 1 July 1974.
| Author | : |
| Publisher | : |
| Total Pages | : 312 |
| Release | : |
| Genre | : |
| ISBN | : |
| Author | : L. A. Marshall |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1967 |
| Genre | : |
| ISBN | : |
| Author | : R. B. Hobbs (Jr.) |
| Publisher | : |
| Total Pages | : 118 |
| Release | : 1967 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
Wind tunnel tests were conducted at M = 10 and at M = 14 and 20 to obtain experimental data on the hypersonic dynamic stability characteristics of a 10-degree half-angle cone. These data were generated to support dynamic stability studies and to evaluate the effects of many geometric and environmental variables, which influence the oscillatory motion of re-entry vehicles. The state-of-the-art of experimental ground testing in hypersonic dynamic stability is reviewed in detail with respect to simulation and data measuring capabilities. Data correlations were obtained to compare facilities and to evaluate the degree of consistency of results using different techniques in measuring and reducing the data. The confidence level for the data is established by means of these correlations, and conclusive interpretations of the data for application in flight estimates can only be made when the significance of these correlations are fully realized. The data correlations do bring out definite inconsistencies in test results and demonstrate the more obvious shortcomings of ground test simulation in this type of experiment research. Test results indicate that the 10-degree cone configuration is dynamically stable over the entire scope of matrix variables covered in the experimental program. Dynamic instabilities observed in flight remain unconfirmed by these ground test results.
| Author | : Dave R. Moore |
| Publisher | : |
| Total Pages | : 90 |
| Release | : 1967 |
| Genre | : Ablation (Aerothermodynamics) |
| ISBN | : |
An experimental program has been conducted in the LTV Hypervelocity Wind Tunnel at M = 17 to investigate the effects of ablation product characteristics and thermal lags on re-entry vehicle dynamic stability. The free oscillation method of dynamic stability measurement was used and the ablation processes were simulated by the controlled mass injection through four sections of the porous model skin. The flow rates through the top and bottom quadrants were oscillated at the same frequency and at an amplitude proportional to the model motion. The thermal lag effect was investigated with nitrogen injection into nitrogen tunnel flow at several different mass flow rates and phase angles between the oscillating mass flow and the body motion. The ablation product study was conducted by injecting gases other than nitrogen with specific heat ratio and molecular weight being the test parameters in addition to mass flow rate. The results obtained from these tests indicate significant effect on dynamic stability with both injection phase angle and some characteristics of the injected gas. The effects of model frequency, Reynolds number and mass injection distribution were also investigated and some static pressure measurements were made near the aft of the model. Appendices to the report contain tabulations of the pertinent data and discussions of supporting analytical studies and data analysis.
