Skip to content

SEARCH · Search NASA

Results for “Trailing edges”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

SourceResearch connectionFrom yearThrough year

Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.

At least 397 records · Page 22

All sources NASA NTRS DOE OSTI

NASA NTRS1948

An Investigation at Low Speed of a 51.3 Degrees Sweptback Semispan Wing with a Raked Tip and with 16.7-percent-chord Ailerons Having Three Spans and Three Trailing-edge Angles

Explore the source record for details and available documents.

Schneiter, Leslie E↗

NASA NTRS1949

Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42.7 Degree Sweptback Wing Model Having an Aileron with Finite Trailing-edge Thickness

Explore the source record for details and available documents.

Lockwood, Vernard E↗

NASA NTRS1949

Control effectiveness and hinge-moment measurements at a Mach number of 1.9 of a nose flap and trailing-edge flap on a highly tapered low- aspect-ratio wing

Explore the source record for details and available documents.

Mitchell, Meade H , Jr↗

NASA NTRS1947

The effectiveness of a trailing-edge spoiler on a swept-back airfoil at transonic speeds from tests by the NACA wing-flow method

Explore the source record for details and available documents.

Silsby, Norman S↗

NASA NTRS1947

Wing-flow Tests of a Triangular Wing of Aspect Ratio Two I : Effectiveness of Several Types of Trailing-edge Flaps on Flat-plate Models

Explore the source record for details and available documents.

FLAPS - COMPLETE WINGS↗

NASA NTRS1949

Two-dimensional Wind-tunnel Investigation of Two NACA 7-series Type Airfoils Equipped with a Slot-lip Aileron, Trailing-edge Frise Aileron, and a Double Slotted Flap

Explore the source record for details and available documents.

Braslow, Albert L↗

NASA NTRS1949

Effects of Systematic Changes of Trailing-edge Angle and Leading-edge Radius on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-percent-chord-thick NACA Airfoil Section

Explore the source record for details and available documents.

Summers, James L↗

NASA NTRS1949

Experimental pressure distributions over wing tips at Mach number 1.9 II : wing tip with subsonic trailing edge

Explore the source record for details and available documents.

Mirels, Harold↗

NASA NTRS1950

Investigation at Mach Number 1.62 of the Pressure Distribution over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap

Explore the source record for details and available documents.

Czarnecki, K R↗

NASA NTRS1950

Measurements of Aerodynamic Characteristics of a 35 Degree Sweptback NACA 65-009 Airfoil Model with 1/4-chord Bevelled-trailing-edge Flap and Trim Tab by the NACA Wing-flow Method

Explore the source record for details and available documents.

Johnson, Harold I↗

NASA NTRS1949

Reduction of Profile Drag at Supersonic Velocities by the Use of Airfoil Sections Having a Blunt Trailing Edge

Explore the source record for details and available documents.

Chapman, Dean R↗

NASA NTRS1950

Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Explore the source record for details and available documents.

Morrow, John D↗

NASA NTRS1950

Effects of Varying the Size and Location of Trailing-edge Flap-type Controls on the Aerodynamic Characteristics of a Unswept Wing at a Mach Number of 1.9

Explore the source record for details and available documents.

Mitchell, Meade H , Jr↗

NASA NTRS1950

Experimental investigation of the mixing loss behind the trailing edge of a cascade of three 90 degree supersonic turning passages

Explore the source record for details and available documents.

Liccini, Luke L↗

NASA NTRS1950

Measurements of the Effect of Trailing-edge Thickness on the Zero-lift Drag of Thin Low-aspect-ratio Wings

Explore the source record for details and available documents.

Morrow, John D↗

NASA NTRS1950

Flight Investigation of the Effect of Thickening the Aileron Trailing Edge on Control Effectiveness for Sweptback Tapered Wings Having Sharp-and Round-nose Sections

Explore the source record for details and available documents.

Strass, H Kurt↗

NASA NTRS1950

High-speed Aerodynamic Characteristics of a Lateral-control Model II : Modified NACA 0012-64 Section with a 26.6-percent-chord, Plain, Trailing-edge Aileron; Wing Unswept and Swept Back 45 Degrees

Explore the source record for details and available documents.

Krumm, Walter J↗

NASA NTRS1950

Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds

Explore the source record for details and available documents.

Thompson, Robert F↗