Similitude Relations for Free-model Wind-tunnel Studies of Store-dropping Problems
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Sandahl, Carl A↗
Engineering topics
Sandahl, Carl A
Publications and source records attributed to Sandahl, Carl A.
Effects of Some Leading-edge Modifications, Section and Plan-form Variations, and Vertical Position on Low-lift Wing Drag at Transonic and Supersonic Speeds
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Welsh, Clement J↗
Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds
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Stoney, William E↗
Effect on Transonic and Supersonic Drag of a Fuselage Protuberance Designed to Improve the Area Distribution of an Essentially Unswept Wing-fuselage Combination
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Sandahl, Carl A↗
Free-flight Investigation of the Zero-lift Drag of Several Wings at Supersonic Mach Numbers Extending to 2.6
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Hopko, Russell N↗
Free-flight Investigation of the Longitudinal Stability and Control of a Rocket-propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails
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Sandahl, Carl A↗
A Comparison of Two Techniques Utilizing Rocket-propelled Vehicles for the Determination of the Damping-in-roll Derivative
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Stone, David G↗
The Rolling Effectiveness of Wing-tip Ailerons as Determined by Rocket-powered Test Vehicles and Linear Supersonic Theory
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Sandahl, Carl A↗
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↗
Rolling Effectiveness of a Thin Tapered Wing Having Partial-span Ailerons as Determined by Rocket-powered Test Vehicles
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Sandahl, Carl A↗
Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds
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Sandahl, Carl A↗
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↗
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of Several Aileron Configurations on a Tapered Wing Having 42.7 Degrees Sweepback
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Sandahl, Carl A↗
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42.7 Degree Sweptback Wing Having Partial-span Ailerons
An investigation of the rolling effectiveness at transonic and supersonic speeds of partial-span ailerons on a 42.7 degree sweptback wing having symmetrical circular-arc airfoil sections of 10-percent thickness ratio normal to the wing quarter-chord line has been made by means of rocket-propelled test vehicles. The results are compared with results of a supersonic wind-tunnel test at Mach number 1.9.
CONTROLS, LATERAL↗
Free-flight Investigation of the Rolling Effectiveness of Several Delta Wing : Aileron Configurations at Transonic and Supersonic Speeds
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Sandahl, Carl A↗
Free-flight Investigation at Transonic and Supersonic Speeds of a Wing-aileron Configuration Simulating the D-558-2 Airplane
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Sandahl, Carl A↗
Preliminary free-flight investigation of the effect of airfoil section on aileron rolling effectiveness at transonic and supersonic speeds
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Sandahl, Carl A↗
Free-flight Investigation of the Rolling Effectiveness of a Wing-spoiler Arrangement at High Subsonic, Transonic, and Supersonic Speeds
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Sandahl, Carl A↗