Wind tunnel tests and flight tests of the Falcon business aircraft were compared. The direct method involves comparing the unitary curves obtained from the two tests, whereas the indirect method consists of establishing from the wind tunnel tests a basic set of adjusted parameters which are converted into the same time based parameters recorded on flight test tapes, using flight mechanic equations and a simulation program. The comparison of the two methods is presented, and the results of longitudinal and lateral tests are discussed.
Comparison of Wind Tunnel Tests and Flight Tests of an Executive Aircraft Comparaison des Essais en Soufflerie et des Essais en Vol pour UN Avion Executive
1975
24 pages
Report
Keine Angabe
Englisch
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