Cover Image

Full-scale span load distribution on tapered wing with split flaps of various spans.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1937.
Subjects:	Aeronautics > Research. Airplanes. Weights and measures.
Online Access:	Electronic resource (PDF)

Similar Items

Calculation of aerodynamic characteristics of tapered wings with partial-span flaps.
Published: (1939)

Span load distribution for tapered wings with partial℗--span flaps.
Published: (1936)

Theoretical span loading and moments of tapered wings produced by aileron deflection.
Published: (1937)

Wind℗--tunnel investigation of tapered wings with ordinary ailerons and partial℗--span split flaps.
Published: (1937)

Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight.
Published: (1939)

Effects of partial-span plain flaps on aerodynamic characteristics of rectangular and tapered Clark Y wing.
Published: (1938)

Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with full-span flap.
Published: (1935)

The effects of partial℗--span slotted flaps on aerodynamic characteristics of a rectangular and a tapered N. A. C. A. 23012 wing.
Published: (1939)

Wind℗-tunnel investigation of rectangular and tapered N. A. C. A. 23012 wings with plain ailerons and full℗-span split flaps.
Published: (1938)

Notes on technique of landing airplanes equipped with wing flaps.
Published: (1936)

Determination of Characteristics of Tapered Wings.
Published: (1936)

Determination of the Mass Moments and Radii of Inertia of the Sections of a Tapered Wing and the Center-of-Gravity Line Along the Wing Span.
Published: (1943)

Wing characteristics as affected by protuberances of short span.
Published: (1932)

Notes on calculation of minimum horizontal tail surface for airplanes equipped with wing flaps.
Published: (1937)

Method of estimating aerodynamic effects of ordinary and split flaps of airfoils.
Published: (1936)

Calculated effect of various types of flap on take-off over obstacles.
Published: (1936)

Flight investigation of lateral control devices for use with full-span flaps.
Published: (1934)

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

Wind℗--tunnel investigation of N. A. C. A. 23012, 23021, and 23030 airfoils with various sizes of split flap.
Published: (1939)

Wind℗--tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps.
Published: (1937)

Influence of tip shape on wing load distribution as determined by flight tests.
Published: (1934)

Empirical corrections to the span load distribution at the tip.
Published: (1937)

The Mean Aerodynamic Chord and the Aerodynamic Center of a Tapered Wing.
Published: (1945)

Tests in variable℗-density wind tunnel of N. A. C. A. 23012 airfoil with plain and split flaps.
Published: (1938)

Wind℗--tunnel tests of wing flaps suitable for direct control of glide-path angle.
Published: (1936)

Design charts for predicting down wash angles and wake characteristics behind plain and flapped wings.
Published: (1938)

Pressure℗--distribution measurements on rectangular wing with partial℗-span split flap in curved flight.
Published: (1939)

Pressure distribution over rectangular airfoil with partial-span split flap.
Published: (1936)

Investigation of full℗--scale split trailing-edge wing flaps with various chords and hinge locations.
Published: (1935)

Relative loading on biplane wings.
Published: (1933)

Relative loading on biplane wings of unequal chords.
Published: (1934)

Downwash and wake behind plain and flapped airfoils.
Published: (1938)

Remarks on elastic axis of shell wings.
Published: (1936)

Theoretical stability and control characteristics of wings with various amounts of taper and twist.
Published: (1938)

Wind-tunnel investigation of N. A. C. A. 23012 airfoil with slotted flap and 3 types of auxiliary flap.
Published: (1938)

Experimental and calculated characteristics of 22 tapered wings [aircraft].
Published: (1937)

Interference on airfoil of finite span in open rectangular wind tunnel.
Published: (1933)

Wing-nacelle℗--propeller interference for wings of various spans, force, and pressure℗--distribution tests.
Published: (1936)

Load tests on stiffened circular cylindrical shell.
Published: (1938)

Wind-tunnel investigation of ground effect on wings with flaps.
Published: (1939)