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| Author | : Frederick P. Povinelli |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1968 |
| Genre | : Gas-liquid interfaces |
| ISBN | : |
| Author | : Frederick P. Povinelli |
| Publisher | : |
| Total Pages | : 19 |
| Release | : 1968 |
| Genre | : Gas-liquid interfaces |
| ISBN | : |
| Author | : Frederick P. Povinelli |
| Publisher | : |
| Total Pages | : |
| Release | : 1968 |
| Genre | : |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1320 |
| Release | : 1966 |
| Genre | : Government publications |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1348 |
| Release | : 1970 |
| Genre | : United States |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 472 |
| Release | : |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 470 |
| Release | : 1969 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 354 |
| Release | : 1968 |
| Genre | : |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1716 |
| Release | : 1968 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
| Author | : David T. Harrje |
| Publisher | : |
| Total Pages | : 668 |
| Release | : 1972 |
| Genre | : Liquid propellant rockets |
| ISBN | : |
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
