Free-flight Pressure Measurements over a Flare-stabilized Rocket Model with a Modified Von Karman Nose for Mach Numbers up to 4.3
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Bland, William M , Jr↗
Engineering topics
Bland, William M , Jr
Publications and source records attributed to Bland, William M , Jr.
Some Effects of Fin Leading-edge Shape on Aerodynamic Heating at Mach Number 2.0 at a Stagnation Temperature of About 2,600 Degrees R
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Bland, William M , Jr↗
Effectiveness of Various Protective Coverings on Magnesium Fins at Mach Number 2.0 and Stagnation Temperatures up to 3,600 Deg R
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Bland, William M , Jr↗
Free-flight Aerodynamic-heating Data to a Mach Number of 15.5 on a Blunted Conical Nose with a Total Angle of 29 Degrees
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Bland, William M , Jr↗
Some experiments with insulated structures
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Rosecrans, Richard↗
Aerodynamic heat transfer to wing surfaces and wing leading edges
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Bond, Aleck C↗
Some Effects of Heat Transfer at Mach Number 2.0 at Stagnation Temperatures Between 2,310 Degrees and 3,500 Degrees R on a Magnesium Fin with Several Leading-edge Modifications
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Bland, William M , Jr↗
Free-flight Aerodynamic-heating Data to Mach Number 10.4 for a Modified Von Karman Nose Shape
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Bland, William M , Jr↗
A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Sting-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings
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Bland, William M , Jr↗
Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing-body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models
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Bland, William M , Jr↗
A Free-flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments
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Bland, William M , Jr↗
Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket Propelled Vehicles
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Bland, William M , Jr↗
Some Effects of Fuselage Interference, Wing Interference, and Sweepback on the Damping in Roll of Untapered Wings as Determined by Techniques Employing Rocket-propelled Vehicles
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Bland, William M , Jr↗
A technique utilizing rocket-propelled test vehicles for the measurement of the damping in roll of sting-mounted models and some initial results of delta and unswept tapered wings
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Bland, William M , Jr↗
Effects of Some Airfoil-section Variations on Wing-aileron Rolling Effectiveness and Drag as Determined in Free Flight at Transonic and Supersonic Speeds
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Sandahl, Carl A↗