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A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models With and Without Tail Fins and Wings

4. TITLE (Continued) 
NUMBER 7, PARTS 2 THEOUGH 105) 
19. KEY WORDS (Continued) 
deflection 
transonic flow 
supersonic flow 
wind tunnel tests 
20. ABSTRACT (Cont inued) 
from 0.20 to 4.63 over an range from —6 to 60 deg 
and a sideslip angle range from —20 to 20 deg for the body—alone 
configurations, body—wing configurations, and the body—wing—tail 
fin configurations .
In addition, the tail fin configurations were 
tested using the reflection plane technique, and the resulting fin 
loads data are presented for a Mach number ra nge of 0.80 to 2.16 
over an angle—of—attack range from O to 210 deg. Volume IV con— 
tains the tabulated data obtained during Test Number 7, Parts 2 
through 105, at the Naval Ship Research and Development Center .

The data presented herein were compiled by the Arnold Engineering Development 
Center (AEDC), Air Force Systems Command (AFSC), under the sponsorship of the Air 
Force Armament Laboratory (AFATL), Eglin Air Force Base, Florida. Seven different 
tests were conducted by three organizations: ARO, Inc. (a subsidiary Of Sverdrup & Parcel 
and Asociates, Inc.), contract operator of the AEDC, AFSC, Amold Air Force Station, 
Tennesee; Naval Ship Research and Development Center (NSRDC), Bethesda, Maryland; 
and Langley Research Center (LRC), National Aeronautics and Space Administration 
(NASA), Langley Air Force Base, Virginia. The data were compiled under ARO Project 
NO. P34A-37A. The author of this report was G. R. Gomillion, ARO, Inc. The manwcript 
(ARO Control No. ARO-PWT-TR-7S-88) was submitted for publication on June 20, 1975.

This volume contairs the tabulated data that were obtained during Test Number 7, 
Parts 2 through 105, that was conducted in the 7 x 10 Foot Transonic Wind Tunnel at 
NSRDC during March 1973. Asan aid in the use of thae data, the table which lists the part 
numbers for the tabulated data from Test Number 7 and the general list of nomenclature are 
repeated from Volume I at the end of this volume.