Drag of a Wing-body Configuration Consisting of a Swept-forward Tapered Wing Mounted on a Body of Fineness Ratio 12 Measured During Free Fall at Transonic Speeds
Explore the source record for details and available documents.
Thompson, Jim Rogers↗
SEARCH · Search NASA
Results for “WINGS - TORSION”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Free-fall Measurements at Transonic Velocities of the Drag of a Wing-body Configuration Consisting of a 45 Degree Swept-back Wing Mounted Forward of the Maximum Diameter on a Body of Fineness Ratio 12
Explore the source record for details and available documents.
Mathews, Charles W↗
Wing-tunnel Investigation at High Subsonic Speeds of the Lateral-control Characteristics of an Aileron and a Stepped Spoiler on a Wing with Leading Edge Swept Back 51.3 Degrees
Explore the source record for details and available documents.
Schneiter, Leslie E↗
Damping-in-roll characteristics of a 42.7 degree sweptback wing as determined from a wind-tunnel investigation of a twisted semispan wing
Explore the source record for details and available documents.
Lockwood, Vernard E↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effects of Split Flaps, Elevons, and Leading-edge Devices at Low Speed
Explore the source record for details and available documents.
Hopkins, Edward J↗
Effects of Wing-tip Turrets on the Aerodynamic Characteristics of a Typical Bomber-wing Model
Explore the source record for details and available documents.
Boddy, Lee E↗
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↗
An Investigation at Low Speed of a Large-scale Triangular Wing of Aspect Ratio Two III : Characteristics of Wing with Body and Vertical Tail
Explore the source record for details and available documents.
Anderson, Adrien E↗
Investigation of Extensible Wing-tip Ailerons on an Untapered Semispan Wing at 0 Degree and 45 Degrees Sweepback
Explore the source record for details and available documents.
Hagerman, John R↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Aerodynamic Characteristics in Sideslip of a Large-scale Model Having a 63 Degree Swept-back Vertical Tail
Explore the source record for details and available documents.
Mccormack, Gerald M↗
Wing-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an All-movable Triangular Wing of Aspect Ratio 4 Alone and with a Body
Explore the source record for details and available documents.
Stivers, Louis S↗
Wing-tunnel Investigation at Low Transonic Speeds of the Effects of Number of Wings on the Lateral-control Effectiveness of an RM-5 Test Vehicle
Explore the source record for details and available documents.
Johnson, Harold S↗
Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models
Explore the source record for details and available documents.
Stone, David G↗
Low-speed Investigation of Deflectable Wing-tip Ailerons on an Untapered 45 Degrees Sweptback Semispan Wing with and Without an End Plate
Explore the source record for details and available documents.
Fischel, Jack↗
Effect of Wing-tank Location on the Drag and Trim of a Swept-wing Model as Measured in Flight at Transonic Speeds
Explore the source record for details and available documents.
Welsh, Clement J↗
Longitudinal Characteristics at Mach Number of 1.24 of 1/30-scale Semispan Model of Bell X-5 Variable-sweep Airplane with Wing Swept Back 60 Degrees : from Tests by NACA Wing-flow Method
Explore the source record for details and available documents.
Silsby, Norman S↗
The Effects of Compressibility on the Pressures on a Body of Revolution and on the Aerodynamic Characteristics of a Wing-nacelle Combination Consisting of the Body of Revolution Mounted on a Swept-back Wing
Explore the source record for details and available documents.
Boltz, Frederick W↗
The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
Explore the source record for details and available documents.
Rathert, George A , Jr↗