Summary and analysis of horizontal-tail contribution to longitudinal stability of swept-wing airplanes at low speeds Page: 1 of 137
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AFR I D 4R TAL Copy N
- -RM L55E2a
SUMMARY AND ANALYSIS OF HORIZONTAL-TAIL CONTRIBUTION
TO LONGITUDINAL STABILI TY OF SWEPT-WING
AIRPLANES AT LOW SPEEDS
By Robert H. Neely and Roland F. Griner
Langley Aeronautical Laboratory
Langley Field, Va.
n,069210 4-' ,c& s (WI 0 1955
, i.,ori.ty o g/" 4 -7 ate/ ..../ 'AjLE(YAERONAUTICAL OLAOATORt
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C~.SSF LD DFCICUINT ANOLV FIELD, VIRGINIA
S This material contains information affecting the National Defense of the United States wi the meaning
of the e.alo-.age laws, Title 18, U.B.C., secs. '23s and '94, the transm:asion or revelation of which i any
-anner to an urauthrized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
m August 23, 1955
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Neely, Robert H. & Griner, Roland F. Summary and analysis of horizontal-tail contribution to longitudinal stability of swept-wing airplanes at low speeds, report, August 23, 1955; (digital.library.unt.edu/ark:/67531/metadc53109/m1/1/: accessed August 18, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.