One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
One-dimensional approach to maximum lift-drag ratio of slender, flat-top, affine wing at hypersonic speeds
FLAT SURFACE↗
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Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Two-dimensional approach to maximum lift-drag ratio of slender, flat-top, wing at hypersonic speeds
FLAT SURFACE↗
Similarity laws for lifting wings of minimum drag at hypersonic speeds
Similarity laws for determining chordwise and spanwise contours minimizing drag of flat-top wing in hypersonic flow
HYPERSONIC FLOW↗
Effect of Several Afterbody Modifications Including Terminal Fairings on the Drag of a Single-engine Fighter Model with Hot-jet Exhaust
Wind tunnel study of drag characteristics of boattailed afterbodies and afterbody terminal fairings for single engine jet aircraft
DRAG EFFECT↗
Shock tube determination of the drag coefficient of small spherical particles
Shock tube determination of drag coefficient of small spherical particles accelerating in laminar, non-reacting, incompressible continuum flow
DRAG COEFFICIENT↗
Effects of bluntness on the subsonic drag of an elliptical forebody
Effects of bluntness on subsonic drag of elliptical forebody
CYLINDRICAL AFTERBODY↗
Phonon-drag thermopower in dilute copper alloys
Phonon-drag thermopower change in dilute copper alloys used to determine numerical values for scattering parameter
SCATTERING↗
Power-law bodies of maximum lift-to-drag ratio in hypersonic flow
Maximizing lift-drag ratio of slender, flat-top, hypersonic body assuming Newtonian pressure distribution and constant skin-friction coefficient
SKIN FRICTION↗
Charts of additive drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack
Charts of additive drag coefficient and mass flow ratio for inlets utilizing right circular cones at zero angle of attack
CHART↗
Definition of lateral-range and lift-drag-ratio requirements for return to both optimum and nonoptimum recovery sites
Lateral range and lift-drag ratio requirements for return to optimum or nonoptimum recovery sites from near-earth circular orbit
LIFT-DRAG RATIO↗
Pressure drags due to two-dimensional fabrication-type surface roughness on an ogive cylinder at transonic speeds
Pressure drags due to two-dimensional fabrication- type surface roughness on ogive cylinder at transonic speeds
CYLINDER↗
A note on the ability to predict transonic drag-rise changes due to model modifications
Wind tunnel test to establish validity of Fourier analysis results for transonic drag rise changes due to model modifications
FOURIER ANALYSIS↗
Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics and drag rise of fighter aircraft
STATIC STABILITY AND CONTROL↗
Minimum Drag of Four Versions of a Swept-wing Fighter Airplane Obtained from Flight Tests of Rocket-boosted Models at Mach Numbers from 0.81 to 1.71
Swept wing fighter aircraft drag coefficient reduction by configuration redesign
AIRCRAFT CONFIGURATION↗
Three-dimensional, lifting wings of minimum drag in hypersonic flow
Three-dimensional lifting wings of minimum drag in hypersonic flow
SLENDER WING↗
Lifting Bodies of Minimum Drag in Hypersonic Flow
Variational calculus methods for drag reduction of lifting bodies in hypersonic flow
DRAG REDUCTION↗
Three-dimensional Wings of Maximum Lift-to- Drag Ratio in Hypersonic Flow
Optimizing lift-to-drag ratio of slender, flat-top wing of given planform in hypersonic flow by using variational calculus methods
LIFT-DRAG RATIO↗
Drag make-up sensor for low-altitude satellites
Satellite drag sensor for controlling low altitude satellite trajectories
SATELLITE DRAG↗