Skip to content

SEARCH · Search NASA

Results for “WINGS - AEROELASTICITY”

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 415 records · Page 23

All sources NASA NTRS DOE OSTI

NASA NTRS1950

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers Form 0.86 to 1.5 of a Wing-body Combination Having a 60 Degree Triangular Wing with NACA 65A003 Sections

Explore the source record for details and available documents.

Nelson, Robert L↗

NASA NTRS1950

Transonic Drag Characteristics of a Wing Body Combination Using a Thin Tapered Wing of 45 Degrees Sweepback

Explore the source record for details and available documents.

Kurbjun, Max C↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Triangular Wing of Aspect Ratio 2 with NACA 0008-63 Section

Explore the source record for details and available documents.

Smith, Donald W↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Triangular Wing of Aspect Ratio 2 with NACA 0005-63 Section

Explore the source record for details and available documents.

Smith, Donald W↗

NASA NTRS1950

Comparison of large scale flight measurements of zero lift drag at Mach numbers from 0.9 to 1.7 of two wing-body combinations having similar 60 degree triangular wings with NACA 65A003 sections

Explore the source record for details and available documents.

Schult, Eugene D↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Triangular Wing of Aspect Ratio 4 with NACA 0005-63 Section

Explore the source record for details and available documents.

Heitmeyer, John C↗

NASA NTRS1951

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0003-63 section

Explore the source record for details and available documents.

Heitmeyer, John C↗

NASA NTRS1951

The Effects of Boundary-layer Control on the Longitudinal Characteristics of a Swept-back Wing Using Suction Through Streamwise Slots in the Outboard Portion of the Wing

Explore the source record for details and available documents.

Mccormack, Gerald M↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-percent-thick, Biconvex Section

Explore the source record for details and available documents.

Reese, David E↗

NASA NTRS1951

Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness at Supersonic Speeds of a 30-percent Chord, 50-percent Semispan Elevon as a Lateral Control Device

Explore the source record for details and available documents.

Olson, Robert N↗

NASA NTRS1951

The Effects of Centrally Mounted Wing-tip Tanks on the Subsonic Aerodynamic Characteristics of a Wing of Aspect Ratio 10 with 35 Degrees of Sweepback

Explore the source record for details and available documents.

Tinling, Bruce E↗

NASA NTRS1951

Flight Measurements of the Wing-dropping Tendency of a Straight-wing Jet Airplane at High Subsonic Mach Numbers

Explore the source record for details and available documents.

Ernst, Edward A↗

NASA NTRS1951

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution

Explore the source record for details and available documents.

Phelps, E Ray↗

NASA NTRS1951

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40

Explore the source record for details and available documents.

Smith, Norman F↗

NASA NTRS1951

Effect of a Deflectable Wing-tip Control on the Low-speed Lateral and Longitudinal Characteristics of a Large-scale Wing with the Leading Edge Swept Back 47.5 Degrees

Explore the source record for details and available documents.

Lange, Roy H↗

NASA NTRS1951

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.8 to 1.6 of a Wing-body Combination Having an Unswept 4.5 Percent Thick Wing with Modified Hexagonal Sections

Explore the source record for details and available documents.

Schult, Eugene D↗

NASA NTRS1951

A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

Explore the source record for details and available documents.

Danforth, Edward C B↗

NASA NTRS1951

Characteristics Throughout the Subsonic Speed Range of a Plane Wing and of a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback

Explore the source record for details and available documents.

Johnson, Ben H , Jr↗