A Note on the Thin-Shock-Layer Approximation
- 1 May 1977
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 28 (2) , 85-89
- https://doi.org/10.1017/s0001925900007988
Abstract
Summary: This Note proposes a restriction on possible solution procedures for thin-shock-layer theory. This restriction has been widely violated in solutions presented hitherto, although with negligible error apparently. Those cases are indicated where failure to apply the restriction leads to definite errors.Keywords
This publication has 4 references indexed in Scilit:
- Some Extensions of Thin-Shock-Layer TheoryAeronautical Quarterly, 1974
- The Effects of Yaw on Conical Wings at High Supersonic SpeedsAeronautical Quarterly, 1970
- Calculated Pressure Distributions and Shock Shapes on Thick Conical Wings at High Supersonic SpeedsAeronautical Quarterly, 1967
- LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORYAIAA Journal, 1963