Accession Number : ADA951630

Title :   On the Feasibility of an Adequate, Fast Response Gust Alleviation System,

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s) : Breuhaus,W. O.

Report Date : 02 SEP 1959

Pagination or Media Count : 19

Descriptors :   *Gusts, *Turbulence, *Supersonic aircraft, Air flow, Aerodynamic forces, Vertical gust recorders, Predictions, Probes, Aerodynamic control surfaces, Low altitude, High velocity

Subject Categories : Aerodynamics
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE