Base Pressure Studies in Rarefied Supersonic Flows
- 1 March 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (3), 193-207
- https://doi.org/10.2514/8.3536
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- An experimental investigation of the interaction between shock waves and boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1954
- Results of Some Base Pressure Experiments at Intermediate Reynolds Numbers with M=2.84Journal of the Aeronautical Sciences, 1954
- Skin Friction in Slip FlowJournal of the Aeronautical Sciences, 1954
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- A Precision Differential ManometerReview of Scientific Instruments, 1952
- A Preliminary Study of Reynolds Number Effects on Base Pressure at M = 2.95*Journal of the Aeronautical Sciences, 1952
- Interrelationship Between Boundary Layer and Base PressureJournal of the Aeronautical Sciences, 1951
- Skin Friction in the Laminar Boundary Layer in Compressible FlowAeronautical Quarterly, 1949
- Superaerodynamics, Mechanics of Rarefied GasesJournal of the Aeronautical Sciences, 1946