Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
Explore the source record for details and available documents.
Lundstrom, Reginald R↗
SEARCH · Engineering Papers
Results for “aspect ratio”
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.
Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
Explore the source record for details and available documents.
Jones, George W , Jr↗
Transonic Flutter Investigation of a Cantilevered, Aspect-ratio-4, 45 Degree Sweptback, Untapered Wing with Three Different Pylon-mounted External-store Configurations
Explore the source record for details and available documents.
Ruhlin, Charle L↗
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered wings at transonic speeds
Explore the source record for details and available documents.
Hammond, Alexander D↗
Investigation at Transonic Speeds of Loading over a 30 Degree Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
Explore the source record for details and available documents.
Arabian, Donald D↗
Effects of Wing Warp on the Lift, Drag, and Static Longitudinal Stability Characteristics of an Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 at Mach Numbers from 1.1 to 1.7
Explore the source record for details and available documents.
Gillespie, Warren, Jr↗
Pressure measurements at transonic and low supersonic speeds on a thin conical cambered low-aspect-ratio delta wing in combination with basic and indented bodies
Explore the source record for details and available documents.
Mugler, John P JR↗
Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 Employing High-velocity Blowing over the Leading- and Trailing-edge Flaps
Explore the source record for details and available documents.
Hickey, David H↗
Flutter and divergence of rectangular wings of very low aspect ratio
Explore the source record for details and available documents.
Fralich, Robert W↗
Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0
Explore the source record for details and available documents.
Peterson, Victor, L↗
The Use of a Leading-edge Area-suction Flap and Leading-edge Modifications to Improve the High-lift Characteristics of an Airplane Model with a Wing of 45 Degree Sweep and Aspect Ratio 2.8
Explore the source record for details and available documents.
Koenig, David G↗
Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
Explore the source record for details and available documents.
Henning, Allen B↗
Experimental and Theoretical Aerodynamic Characteristics of Two Low-aspect-ratio Delta Wings at Angles of Attack to 50 Degrees at a Mach Number of 4.07
Explore the source record for details and available documents.
Smith, Fred M↗
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating near the Free Water Surface
Explore the source record for details and available documents.
Johnson, Virgil E , Jr↗
Experimental Lift of Low-aspect-ratio Triangular Wings at Large Angles of Attack and Supersonic Speeds
Explore the source record for details and available documents.
Hill, William A , Jr↗
An Investigation of the Control Effectiveness of Tip Ailerons and Spoilers on a Low-aspect-ratio Trapezoidal-wing Airplane Model at Mach Numbers from 1.55 to 2.35
Explore the source record for details and available documents.
Wong, Norman D↗
Transonic Investigation of Yawed Wings of Aspect Ratios 3 and 6 with a Sears-haack Body and with Symmetrical and Asymmetrical Bodies Indented for a Mach Number of 1.20
Explore the source record for details and available documents.
Holdaway, George H↗
Effect of Control Trailing-edge Thickness or Aspect Ratio on the Oscillating Hinge-moment and Flutter Characteristics of a Flap-type Control at Transonic Speeds
Explore the source record for details and available documents.
Moseley, William C , Jr↗