A brief description of the GA (W) -2 Airfoil Flight Test Evaluation Program is presented. Employing an economical approach to airfoil flight testing, the GA (W) -2 airfoil was “gloved” on the existing wing structure of a Beech Model C23 “Sundowner”. Program objectives, experimental approach, research aircraft modification and instrumentation, data acquisition and processing, flight operations, and preliminary flight test results are described.
GA(W)-2 Airfoil Flight Test Evaluation
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1976
01.02.1976
Aufsatz (Konferenz)
Englisch
Flight test techniques for low speed airfoil evaluation
NTRS | 1978
|Airfoil System for Cruising Flight
NTRS | 2014
|A DATA ACQUISITION SYSTEM FOR IN-FLIGHT AIRFOIL EVALUATION
SAE Technical Papers | 1976
|Measurements of airfoil resistance in flight
Engineering Index Backfile | 1928
|