Computational aerodynamics has evolved to be a practical design tool comparable to wind tunnel testing, and it has played an important role in actual aircraft design stages. There have been intensive works already done for code validation to support the accuracy of the computation. The code accuracy based upon comparison between numerical simulation and actual flight test is discussed for the first time.
Comparative Study on Wing Pressure Distribution of High Speed Jet Airplane Between Numerical Simulation and Flight Test
1989
6 pages
Report
Keine Angabe
Englisch
Airplane configurations for high speed flight
Engineering Index Backfile | 1954
|FLIGHT TEST RESULTS FOR AN ADVANCED TECHNOLOGY LIGHT AIRPLANE WING
SAE Technical Papers | 1974
|Airplane configurations for high speed flight
Engineering Index Backfile | 1953
|Airplane configurations for high speed flight
Engineering Index Backfile | 1953
|