Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01 Page: 1 of 83
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LONGITUDINAL STABILITY INVESTIGATION
OF A VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE
CONFIGURATION WITH SIMULATED JET INTAKE AND EXHAUST
AT MACH NUMBERS OF 1.61 AND 2.01
By Douglas R. Lord
Langley Aeronautical Laborato
R. ~Langley Field, Va.
JAN 30 1bb
. ' -LANGLEY AERONAUTICAL LABORATORY
J ..ANGLEY rtn.v, vtRUINIA
This material contains information affecting the National Defense of the United States within the meaning
i of the espionage laws, Title 18, U.S.C., Secs. 793 and 794, the transmission or revelation of which in any
manner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
January 30, 19:58
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Lord, Douglas R. Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01, report, January 30, 1958; (https://digital.library.unt.edu/ark:/67531/metadc64021/m1/1/: accessed April 20, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.