Accession Number:

AD0256515

Title:

LOW-SPEED INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE OF OSCILLATION IN SIDESLIP ON THE LATERAL STABILITY DERIVATIVES OF A 60 DEGREE DELTA WING, A 45 DEGREE SWEPTBACK WING, AND AN UNSWEPT WING

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Report Date:

1961-05-01

Pagination or Media Count:

1.0

Abstract:

This investigation was made for values of the reduced-frequency parameter of 0.066 and 0.218 and for a range of amplitudes from plus or minus 2 degrees to plus or minus 6 degrees. The results indicated that the effect of frequency manifests itself mainly in the high angle-of-attack region and that the 60 degree delta wing exhibited the largest effect, whereas the unswept wing exhibited the smallest effect. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE