Max Kramer

Lateral Control by Spoilers at the DVL

Max Kramer, Theodor W Zobel, C. G. Esche, 1951 .

Increase in the maximum lift of an airplane wing due to a sudden increase in its effective angle of attack resulting from a gust

Max Kramer, 1932 .

The Aerodynamic Profile as Acoustic Noise Generator

Max Kramer, 1953 .