Cover Image

Comparison of Automatic Control Systems.

Bibliographic Details
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1941.
Subjects:	Aeronautics > Research. Measuring instruments. Mathematics. Airplanes.
Online Access:	Electronic resource (PDF)

Similar Items

Supplement to Comparison of Automatic Control Systems.
Published: (1941)

Comparison of Automatic Control Systems.
Published: (1941)

Supplement to Comparison of Automatic Control Systems.
Published: (1941)

DFS Dive-Control Brakes for Gliders and Airplanes.
Published: (1940)

Aerodynamics of Rotating-Wing Aircraft with Blade-Pitch Control.
Published: (1940)

The Shcok-Absorbing System of the Airplane Landing Gear.
Published: (1940)

General Relationships Between the Various Systems of Reference Axes Employed in Flight Mechanics.
Published: (1940)

Air Transport by Gliders, Some Technical Observations.
Published: (1941)

Statistical Analysis of the Time and Fatigue Strength of Aircraft Wing Structures.
Published: (1941)

On the Calculation of Flow Past an Infinite Screen on Thin Airfoils.
Published: (1941)

Contribution to the Aerodynamics of Rotating Wing Aircraft.
Published: (1941)

General Airfoil Theory.
Published: (1941)

The Elliptic Wing Based on the Potential Theory.
Published: (1941)

Observations of the Effect of Wing Appendages and Flaps on the Spread of Seperation of Flow Over the Wing.
Published: (1941)

The Oscillating Wing with Aerodynamically Balanced Elevator.
Published: (1941)

Propeller Blade Stresses Caused by Periodic Displacement of the Propeller Shaft.
Published: (1942)

Stresses in Single-Spar Wing Constructions with Incompletely Built-Up Ribs.
Published: (1940)

Two-Dimensional Potential Flow Past an Ordinary Thick Wing Profile.
Published: (1942)

Measurements and Analysis of the Motion of a Canard Airplane Model in Gusts, Apr. 1940.
Published: (1940)

Pressure Distribution on Wings in Reversed Flow.
Published: (1942)

Effect of Wing Loading, Aspect Ratio, and Span Loading on Flight Performances.
Published: (1940)

Wind-Tunnel Investigation of Two Airfoils with 25-Percent-Chord Gwinn and Plain Flaps, May 1940.
Published: (1940)

Experimental Results with Airfoils Tested in the High-Speed Tunnel at Guidonia.
Published: (1940)

Chordwise Load Distrubution of Simple Rectangular Wing.
Published: (1940)

Theoretical Solution to Profile Drag.
Published: (1942)

Pressure-Distribution Investigation of an N.C.A.A. 0009 Airfoil with an 80-Percent Chord Plain and Three Tabs, May 1940.
Published: (1940)

Prediction of Downwash and Dynamic Fluid at the Tail from Free-Flight Measurements.
Published: (1942)

Statics of Circular Stiffeners for Monocoque Fuselages.
Published: (1942)

Buckling Tests with Spar-Rib Grill.
Published: (1940)

A Simple Approximation Method for Observing the Spanwise Lift Distribution.
Published: (1940)

Flow Around Wings Accompanied by Seperation of Vortices.
Published: (1940)

Diagrams for Calculation of Airfoil Lattices.
Published: (1942)

Chart for Critical Compressive Stress of Flat Rectangular Planes, Aug. 1940.
Published: (1940)

The Compressible Potential Flow Past Elliptic Symmetrical Cylinders at Zero Angle of Attack and with No Circulation.
Published: (1942)

New Method of Extrapolation of the Resistance of a Model Planing Boat to Full Size.
Published: (1942)

The Strength of Shell and Tubular Spar Wings.
Published: (1940)

Pressure-Distribution Investigation of an N.C.A.A. 0009 Airfoil with a 30-Percent Chord Plain Flap and Three Tabs, May 1940.
Published: (1940)

Statistical Analysis of Service Stresses on Aircraft Wings.
Published: (1942)

Constibution to the Ideal Efficiency of Screw Propellers.
Published: (1942)

Strength Tests on Hulls and Floats.
Published: (1942)