Two different aircraft designs, each with two modified fuel control systems, were evaluated. Each aircraft was evaluated in a given series of defined ground and flight conditions while quantitative and qualitative observations were made. During this program, some ten flights were completed, and a total of about 13 hours of engine run time was accumulated by the two airplanes. The results of these evaluations with emphasis on the operational and safety aspects were analyzed. Ground tests of the engine alone were not able to predict acceptable limiting lean mixture settings for the flight envelopes of the Cessna Models 150 and T337.
Flight test summary of modified fuel systems
1976-09-01
Conference paper
No indication
English
British Library Conference Proceedings | 2007
|XB -70 Flight Test Summary, Flight 1-6
NTIS | 2022
|AFTI/F-111 Performance Flight Test Summary
SAE Technical Papers | 1987
|Pilot's summary of XB-70 flight test experience
Engineering Index Backfile | 1966
|B-70 Flight Test Summary, Flight 1-7 4 MARCH 1965
NTIS | 2022
|