Aerodynamic design integration of supersonic aircraft
Supersonic aerodynamic design tools, discussing technological application of high speed computer and limitations
Baals, D. D.↗
Engineering topics
Harris, R. V., Jr.
Publications and source records attributed to Harris, R. V., Jr..
Aerodynamic design integration of supersonic aircraft.
Supersonic aerodynamic design tools, discussing technological application of high speed computer and limitations
Baals, D. D.↗
Program computes zero lift wave drag of entire aircraft
Computer program computes zero lift wave drag of an entire aircraft including any combination of the wing, body, pods, fins, and carnard. The program computes the external volume of the wing and the axial area distribution of the wing equivalent body.
Craidon, C. B.↗
Supersonic aircraft Patent
Design of supersonic aircraft with novel fixed, swept wing planform
Carlson, H. W.↗
Recent research results in the aerodynamics of supersonic vehicles.
Analytic processes for evaluation of supersonic aerodynamics of configuration treating drag, wing design, warp, interference and sidewash
AERODYNAMICS↗
A numerical technique for analysis of wave drag at lifting conditions
Numerical technique for analysis of wave drag at lifting conditions for supersonic aircraft
SUPERSONIC AIRCRAFT↗
Use of grit-type boundary-layer transition trips on wind-tunnel models
Guidelines applicable to grit-type boundary layer transition trips near leading edges of wind tunnel models
BOUNDARY LAYER TRANSITION↗
Cruise performance and stability considerations for jet V/STOL aircraft
Cruise performance and aerodynamic stability characteristics of multimission jet V/STOL AIRCRAFT
AERODYNAMIC STABILITY↗
A numerical technique for analysis of wave drag at lifting conditions
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Harris, R. V., Jr.↗
Drag characteristics of a series of low-drag bodies of revolution at Mach numbers from 0.6 to 4.0
Drag characteristics of low drag bodies of revolution at Mach numbers from 0.6 to 4.0
DRAG↗
Recent research results in the aerodynamics of supersonic vehicles.
Analytic processes for evaluation of supersonic aerodynamics of configuration treating drag, wing design, wrap, interference and sidewash
SUPERSONIC AIRCRAFT↗
Recent Research Results in the Aerodynamics of Supersonic Vehicles
Wave drag, drag due to lift and aerodynamic interference effects on efficiency of supersonic cruise vehicle
AERODYNAMIC CHARACTERISTICS↗
Effects of distributed roughness height on aerodynamic characteristics and boundary- layer transition of a wing-body-tail configuration at a mach number of 1.61
Effects of three dimensional roughness trips on aerodynamic characteristics and boundary layer transition of wing-body-tail configuration
ROUGHNESS↗
EFFECTS OF PEAK DECELERATION ON RANGE SENSITIVITY FOR A MODULATEDLIFT REENTRY AT SUPERCIRCULAR SPEEDS
Effects of peak deceleration on range sensitivity for modulated lift reentry
DECELERATION↗
Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01
Effect of canted forward faces on static longitudinal stability characteristics of escape and exit configurations of Mercury capsule at Mach 2.01
LONGITUDINAL STABILITY AND CONTROL↗
Static Longitudinal Stability Characteristics at a Mach Number of 1.98 of a Nonlifting- Space-capsule Model with Finned-adapter Escape System
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Harris, R. V., Jr.↗