On Heat Transfer, Recovery Factors, and Spin for Laminar Flows
- 1 November 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (11) , 787-789
- https://doi.org/10.2514/8.2472
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Recovery Factors for the Laminar "Separation" and Stagnation FlowsJournal of the Aeronautical Sciences, 1952
- Heat Transfer to Constant-Property Laminar Boundary-Layer Flows with Power-Function Free-Stream Velocity and Wall-Temperature VariationJournal of the Aeronautical Sciences, 1952
- On the Flight Dynamics of Slender Special-Purpose AircraftJournal of the Aeronautical Sciences, 1952
- On the Solution of Total Differential, Boundary Value ProblemsJournal of the Aeronautical Sciences, 1951
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949
- Automatic Integration of Linear Second-Order Differential Equations by Means of Punched Card MachinesReview of Scientific Instruments, 1941