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Sidney M Harmon

Observed names: Harmon, S. M., Harmon, Sidney M, Harmon, Sidney M.
OpenAlex ID: A5067971638
Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges
1950 · Sidney M Harmon, Isabella Jeffreys · NASA STI Repository (National Aeronautics and Space Administration) · 20
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Stability Derivatives at Supersonic Speeds of Thin Rectangular Wings with Diagonals Ahead of Tip Mach Lines
1949 · Sidney M Harmon · NASA Technical Reports Server (NASA) · 8
Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
1949 · Sidney M Harmon · NASA Technical Reports Server (NASA) · 5
Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
1947 · Sidney M Harmon · NASA STI Repository (National Aeronautics and Space Administration) · 5
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Calculations of the supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio : wings swept behind the Mach lines
1947 · Sidney M Harmon, Margaret D Swanson · NASA STI Repository (National Aeronautics and Space Administration) · 3
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Stability derivatives of thin rectangular wings at supersonic speeds : wing diagonal ahead of tip mach lines
1948 · Sidney M Harmon · NASA STI Repository (National Aeronautics and Space Administration) · 1
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Comparison of fixed-stabilizer, adjustable- stabilizer and all-movable horizontal tails
1945 · Sidney M Harmon · NASA Technical Reports Server (NASA) · 1
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Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds
1951 · Sidney M Harmon · Defense Technical Information Center (DTIC)
Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds
1951 · Sidney M Harmon · NASA Technical Reports Server (NASA)
Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges
1950 · Sidney M Harmon, John C. Martin · Defense Technical Information Center (DTIC)
NACA Technical Reports
1948 · Harmon, Sidney M. · University of North Texas Digital Library (University of North Texas)
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NACA Technical Notes
1947 · Harmon, Sidney M., Martin, John C. · University of North Texas Digital Library (University of North Texas)
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NACA Research Memorandums
1947 · Harmon, Sidney M., Swanson, Margaret D. · University of North Texas Digital Library (University of North Texas)
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
1945 · Sidney M Harmon · University of Florida Digital Collections (University of Florida)
NACA Advanced Confidential Reports
1945 · Harmon, S. M. · University of North Texas Digital Library (University of North Texas)
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Determination of the damping moment in yawing for tapered wings with partial-span flaps
1943 · Sidney M Harmon · NASA Technical Reports Server (NASA)
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Additional design charts relating to the stalling of tapered wings
1943 · Sidney M Harmon · NASA Technical Reports Server (NASA)
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A Study of the Effect of Increased Size and Speed of Pursuit Airplanes on the Aileron Balancing Problem
1942 · Hartley A Soule, Sidney M Harmon · NASA Technical Reports Server (NASA)
Investigation of means for extending the range of several bombers to 6000 miles
1942 · Sidney M Harmon · NASA STI Repository (National Aeronautics and Space Administration)
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NACA Memorandum Reports
1942 · Ribner, H. S., Harmon, S. M. · University of North Texas Digital Library (University of North Texas)
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Aerodynamic factors affecting the ability of a pilot to return an airplane to level from a banked attitude by use of the rudder alone and without change of heading
1941 · Sidney M Harmon · NASA Technical Reports Server (NASA)
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NACA Advanced Restricted Reports
1941 · Harmon, S. M. · University of North Texas Digital Library (University of North Texas)
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Works count: 26
Citation count: 43
H-index: 4
I10-index: 1
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