Readers Forum
- 1 February 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (2) , 177-192
- https://doi.org/10.2514/8.3527
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- Separation of a Supersonic Turbulent Boundary LayerJournal of the Aeronautical Sciences, 1955
- EditorsJournal of Jet Propulsion, 1954
- The Estimation of Normal-Force, Drag, and Pitching-Moment Coefficients for Blunt-Based Bodies of Revolution at Large Angles of AttackJournal of the Aeronautical Sciences, 1954
- Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic FlowJournal of the Aeronautical Sciences, 1954
- Transformation Between Compressible and Incompressible Boundary-Layer EquationsJournal of the Aeronautical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- The Compressible Boundary LayerJournal of the Aeronautical Sciences, 1952
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949
- Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1938
- LXVI. On the correction for shear of the differential equation for transverse vibrations of prismatic barsJournal of Computers in Education, 1921