Accession Number:

AD0919645

Title:

Aerodynamic Control Effectiveness of a Cruciform Trailing Edge Controlled Vehicle at High Subsonic Mach Numbers Using Individual Flap Effectiveness. Book 1.

Personal Author(s):

Corporate Author:

AIR FORCE ARMAMENT LAB EGLIN AFB FL

Report Date:

1974-04-01

Abstract:

This report documents the technique and results of describing the aerodynamic control effectiveness of a cruciform trailing edge controlled vehicle using the effectiveness of each of the four control surfaces. It is shown that one or two flaps can be used to obtain data in the wind tunnel, and equations can then be used to relate those data to the other flaps not tested. This report consists of two books. Book 1 contains the basic text and Appendixes A to F. Book 2 contains Appendixes G to L. Author

Descriptive Note:

Final rept. Oct 73-Apr 74,

Supplementary Note:

See also Book 2, AD-919 646L.

Pages:

0278

File Size:

0.00MB

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