The braking system for a short takeoff aircraft is discussed and the deficiencies are described. The installation of a Boeing 727 aircraft brake system was made to correct the deficiencies. Tests of the modified system were conducted using an analog computer/hardware simulator. Actual performance tests were conducted and the characteristics of the system were satisfactory.
Brake control system modification, augmentor Wing Jet STOL Research Airplane (AWJSRA)
1974-06-24
Report
No indication
English
The Augmentor Wing - A new approach to jet STOL.
NTRS | 1967
|The augmentor wing - Powered-lift STOL a proven concept
NTRS | 1974
|