THE INFLUENCE OF AIRPLANE CONFIGURATION ON SONIC-BOOM CHARACTERISTICS
Dependence of sonic boom overpressures on supersonic aircraft configurations and design aspects to minimize boom
SUPERSONIC AIRCRAFT↗
Engineering topics
Carlson, H. W.
Publications and source records attributed to Carlson, H. W..
The influence of airplane configuration on sonic-boom characteristics
Effect of aircraft configuration on sonic boom overpressures
AIRCRAFT CONFIGURATION↗
Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01
Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wing-body combinations
TRAPEZOIDAL WING↗
A wind-tunnel investigation of some aspects of the supersonic boom
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Carlson, H. W.↗
The aerodynamics of the supersonic boom
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Carlson, H. W.↗
Experimental and Theoretical Determination of Forces and Moments on a Store and on a Store- Pylon Combination Mounted on a 45 Deg Swept- Wing-Fuselage Configuration at a Mach Number of 1.61
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in supersonic pressure tunnel
PYLON MOUNTING↗
Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-release Motions
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Carlson, H. W.↗
CALCULATION OF EXTERNAL-STORE LOADS AND CORRELATION WITH EXPERIMENT
Calculation of external-store loads and correlation with experiment
EXTERNAL STORE↗
Measurement of static forces on externally carried bombs of fineness ratios 7.1 and 10.5 in the flow field of a swept-wing fighter- bomber configuration at a Mach number of 1.6
Static force and interference drag on externally carried bomb in flow field of supersonic, swept wing fighter-bomber aircraft
SUPERSONIC SPEED↗
THE ORIGIN AND DISTRIBUTION OF SUPSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. V - SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE. MACH NUMBER 2.01
Origin & distribution of supersonic store interference/measurement of individual forces - swept-wing heavy bomber with large store figure
EXTERNAL STORE↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. III - SWEPT-WING FIGHTER-BOMBER CONFIGURATION WITH LARGE AND SMALL STORES. MACH NUMBER, 1.61
Origin of supersonic store interference from measurements of individual forces - swept-wing fighter-bomber with large & small stores
EXTERNAL STORE↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGE-STORE CONFIGURATIONS. II - SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE. LATERAL FORCES AND PITCHING MOMENTS, MACH NUMBER, 1.61
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moments
SWEPT WING↗
THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. 1.-SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE . LIFT AND DRAG, MACH NUMBER, 1.61
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
EXTERNAL STORE↗
Experimental techniques for predicting store motions during release or ejection
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Faget, M. A.↗