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Carl A Sandahl

Observed names: CARL SANDAHL, Sandahl, Carl, Sandahl, Carl A, Sandahl, Carl A.
OpenAlex ID: A5084760323
Similitude Relations for Free-model Wind-tunnel Studies of Store-dropping Problems
1957 · Carl A Sandahl, Maxime A Faget · 4
Free-flight Investigation of Control Effectiveness of Full-span 0.2-chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Section Thickness and Wing Sweepback
1947 · Carl A Sandahl, Alfred A Marino · 3
The Rolling Effectiveness of Wing-Tip Ailerons as Determined by Rocket-Powered Test Vehicles and Linear Supersonic Theory
1950 · Carl A Sandahl, H Kurt Strass, et al. · 2
Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds
1949 · Carl A Sandahl, H Kurt Strass · NASA STI Repository (National Aeronautics and Space Administration) · 2
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Additional Results in a Free-flight Investigation of Control Effectiveness of Full-span, 0.2-chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickne
1948 · Carl A Sandahl, H Kurt Strass · NASA STI Repository (National Aeronautics and Space Administration) · 2
Wind-tunnel investigation of effects of a pusher propeller on lift, profile drag, pressure distribution, and boundary-layer transition of a flapped wing
1945 · Carl A Sandahl · University of Florida Digital Collections (University of Florida) · 2
The Effect of Nose Shape on the Drag of Bodies of Revolution at Zero Angle of Attack
1951 · A. Seiff, Carl A Sandahl · NASA Technical Reports Server (NASA) · 1
A Comparison of Two Techniques Utilizing Rocket-propelled Vehicles for the Determination of the Damping-in-roll Derivative
1951 · David G Stone, Carl A Sandahl · 1
Free-Flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42.7 Degree Sweptback Wing Having Partial-Span Ailerons
1948 · Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration) · 1
The unguided solid rocket for aerodynamic testing.
1965 · James L. Raper, Carl A Sandahl · NASA Technical Reports Server (NASA)
Current Status of the Solid-propellant Flight- Test Vehicle
1964 · CARL SANDAHL, JAMES RAPER · AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Effects of Some Leading-edge Modifications, Section and Plan-form Variations, and Vertical Position on Low-lift Wing Drag at Transonic and Supersonic Speeds
1955 · Clement J. Welsh, Harvey A Wallskog, et al.
Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds
1954 · William E Stoney, Carl A Sandahl · NASA Technical Reports Server (NASA)
Effect on Transonic and Supersonic Drag of a Fuselage Protuberance Designed to Improve the Area Distribution of an Essentially Unswept Wing-fuselage Combination
1954 · Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration)
Effect on transonic and supersonic drag of a fuselage protuberance of an essential unswept wing-fuselage combination
1954 · Carl A Sandahl
Free-Flight Investigation of the Zero-Lift Drag of Several Wings at Supersonic Mach Numbers Extending to 2.6
1952 · Russell N Hopko, Carl A Sandahl
NACA Research Memorandums
1951 · Seiff, Alvin, Sandahl, Carl A., et al. · University of North Texas Digital Library (University of North Texas)
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Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails
1950 · James R. Hall, Carl A Sandahl
Rolling effectiveness of a thin tapered wing having partial-span ailerons as determined by rocket-powered test vehicles
1950 · Carl A Sandahl, H Kurt Strass
The Zero-Lift Drag of Several Configurations of the XAAM-N-2 Pilotless Aircraft. TED No. NACA DE332
1950 · James R. Hall, Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration)
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Effects of some airfoil-section variations on wing-aileron rolling effectiveness and drag as determined in free flight at transonic and supersonic speeds
1949 · Carl A Sandahl, William M Bland, et al.
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
1949 · Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration)
Control-surface characteristics at transonic speeds
1949 · John G Lowry, Carl A Sandahl · NASA Technical Reports Server (NASA)
Free-flight Investigation of the Rolling Effectiveness of Several Delta Wing : Aileron Configurations at Transonic and Supersonic Speeds
1948 · Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration)
Free-flight Investigation at Transonic and Supersonic Speeds of a Wing-aileron Configuration Simulating the D-558-2 Airplane
1948 · Carl A Sandahl · NASA STI Repository (National Aeronautics and Space Administration)
Works count: 46
Citation count: 18
H-index: 2
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