The estimation of aerodynamic forces on flat plate aerofoils at hypersonic and supersonic speed

Autor: J. L. Stollery, S. Punniyakotti
Rok vydání: 2012
Předmět:
Zdroj: The Aeronautical Journal. 116:1207-1215
ISSN: 2059-6464
0001-9240
DOI: 10.1017/s0001924000007570
Popis: Existing theories are reviewed and compared. From the Tangent Wedge formula a simple expression for the normal force on thin wings is derived and compared with some existing experimental data, which cover the whole supersonic-hypersonic range of Mach numbers.
Databáze: OpenAIRE