Wind-Tunnel Sonic-Boom Testing Techniques
Wind tunnel tests of sonic boom phenomena, noting weak pressure field measurement, construction of extremely small models, boundary layer effects, etc
TEST METHOD↗
Engineering topics
Carlson, H. W.
Publications and source records attributed to Carlson, H. W..
Supersonic aircraft Patent
Design of supersonic aircraft with novel fixed, swept wing planform
Carlson, H. W.↗
Experimental and analytic research on sonic boom generation at NASA
NASA research on sonic boom generation /review/
Carlson, H. W.↗
Sonic-boom characteristics of proposed supersonic and hypersonic airplanes
Sonic boom characteristics of proposed supersonic and hypersonic aircraft
SONIC BOOM↗
Wind-Tunnel Sonic-Boom Testing Techniques
Wind tunnel tests of sonic boom phenomena, noting weak pressure field measurement, construction of extremely small models, boundary layer effects, etc
WIND TUNNEL↗
Sonic-boom pressure-field estimation techniques.
Digital computer utilization to estimate sonic boom characteristics of complex airplane configuration
SONIC BOOM↗
Nomograms for determining sonic-boom overpressure.
Nomograms for rapid calculation of maximum ground sonic-boom overpressure for different flight conditions
SUPERSONIC FLIGHT↗
Current methods for prediction and minimization of lift-induced drag at supersonic speeds
Explore the source record for details and available documents.
Carlson, H. W.↗
Sonic boom characteristics of proposed supersonic and hypersonic airplanes
Explore the source record for details and available documents.
Mclean, F. E.↗
A numerical method for calculating near-field sonic-boom pressure signatures
Numerical method for calculating near field sonic room pressure signatures and application to high speed digital computer programming
SONIC BOOM↗
A wind-tunnel investigation of the effect of body shape on sonic-boom pressure distributions
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distributions
WIND TUNNEL↗
The influence of airplane configuration on the shape and magnitude of sonic-boom pressure signatures.
Airplane configuration effect on shape and magnitude of sonic boom pressure signature, noting theoretical and empirical methods
AIRCRAFT CONFIGURATION↗
Numerical method of estimating and optimizing supersonic aerodynamic characteristics of arbitrary planform wings.
Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics
PRESSURE DISTRIBUTION↗
Prediction of airplane sonic-boom pressure fields
Sensitivity of supersonic-transport design and operation to sonic boom
SUPERSONIC TRANSPORT↗
Correlation of sonic-boom theory with wind-tunnel and flight measurements
Correlation of sonic boom theory with wind tunnel and flight measurements
WIND TUNNEL↗
A numerical method of estimating and optimiz- ing the supersonic aerodynamic characteristics of wings of arbitrary planform
Numerical method for pressure distribution on flat wing of arbitrary planform
WING PLANFORM↗
Influence of airplane configuration on sonic- boom characteristics
Wind tunnel and flight testing of airplane configuration influence on sonic boom characteristics
FLIGHT TEST↗