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Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42 / by Schuldenfrei, Marvin
Published 1951Call Number: Loading…
Located: Loading…Government Document Book Loading… -
2
Wind-tunnel investigagion of an NACA 23012 airfoil with a Handley Page slat and two flap arrangements / by Schuldenfrei, Marvin
Published 1942Call Number: Loading…
Located: Loading…Government Document Book Loading… -
3
Some notes on the determination of the stick-free neutral point from wind-tunnel data / by Schuldenfrei, Marvin
Published 1944Call Number: Loading…
Located: Loading…Government Document Book Loading… -
4
Some notes on the determination of the stick-fixed neutral point from wind-tunnel data / by Schuldenfrei, Marvin
Published 1943Call Number: Loading…
Located: Loading…Government Document Book Loading… -
5
Jet-boundary corrections to the downwash behind powered models in rectangular wind tunnels with numerical values for 7- by 10-foot closed wind tunnels / by Swanson, Robert S.
Published 1942Other Authors: “…Schuldenfrei, Marvin…”
Call Number: Loading…
Located: Loading…Government Document Book Loading… -
6
Wind-tunnel investigation of a plain and a slot-lip aileron on a wing with a full-span flap consisting of an inboard Fowler and an outboard slotted flap / by Rogallo, Francis M. (Francis Melvin), 1912-2009
Published 1941Other Authors: “…Schuldenfrei, Marvin…”
Call Number: Loading…
Located: Loading…Government Document Book Loading… -
7
Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps / by Swanson, Robert S.
Published 1941Other Authors: “…Schuldenfrei, Marvin…”
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Located: Loading…Government Document Book Loading…
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Related Subjects
Airplanes
Charts, diagrams, etc
Wind tunnel testing
Aerofoils
Wings
Mathematics
Center of mass
Control
Control surfaces
Flaps (Airplanes)
Stability of airplanes, Longitudinal
Testing
Ailerons
Air flow
Control systems
Downwash (Aerodynamics)
Elevators (Airplanes)
Equations
Lift (Aerodynamics)
Models
Slotted flaps (Airplanes)
Split flaps (Airplanes)
Stability of airplanes, Lateral
Tail surfaces