Inviscid flow about airfoils at high supersonic speeds /
The flow about curved airfoils is investigated analytically at high supersonic speeds assuming air behaves first as an ideal, and then as a calorically imperfect gas. For ideal gas flows it is shown that the shock-expansion method accurately predicts pressure distributions on curved airfoils at arbi...
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1952]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2646 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
ISIL:US-CST NACA TN 2646 |
|---|