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Influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces / by Wolhart, Walter D.
Published 1951Call Number: Loading…
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2
Static longitudinal and lateral stability characteristics at low speed of unswept-midwing models having wings with an aspect ratio of 2, 4, or 6 / by Wolhart, Walter D.
Published 1956Call Number: Loading…
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3
Static longitudinal and lateral stability characteristics at low speed of 60 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6 / by Wolhart, Walter D.
Published 1958Call Number: Loading…
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4
Experimental investigation of the low-speed static and yawing stability characteristics of a 45 degree sweptback high-wing configuration with various twin vertical wing fins / by Goodman, Alex
Published 1951Other Authors: “…Wolhart, Walter D.…”
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5
Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree... by Queijo, M. J.
Published 1950Other Authors: “…Wolhart, Walter D.…”
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6
Some effects of amplitude and frequency on the aerodynamic damping of a model oscillating continuously in yaw / by Fisher, Lewis R.
Published 1952Other Authors: “…Wolhart, Walter D.…”
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7
Static longitudinal and lateral stability characteristics at low speed of 45 degrees sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6 / by Thomas, David F.
Published 1957Other Authors: “…Wolhart, Walter D.…”
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8
Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058
Published 1952Other Authors:Call Number: Loading…Online Access
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Related Subjects
Airplanes
Stability of airplanes, Lateral
Wings, Swept-back
Models
Stability of airplanes, Longitudinal
Stability of airplanes
Tail surfaces
Testing
Wind tunnel testing
Wings
Yawing (Aerodynamics)
Aeronautics
Aircraft engines
Aircraft parts
Aspect ratio (Aerofoils)
Damping
Fuselage
Rolling (Aerodynamics)
Transportation research
Vibration (Aeronautics)