Design trends for Army/Air Force airplanes in the United States / M. Leroy Spearman von Spearman, M. Leroy

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Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 / by M. Leroy Spearman and Ida K. Collins von Spearman, M. Leroy

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Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at mach 1.60 to 2.87 / Leroy Spearman and Willian J. Monta von Spearman, M. Leroy

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Stability and control characteristics at a mach number of 2.01 of a supersonic VTOL airplane model having a broad fuselage and small delta wings / by Cornelius Driver and M. Leroy Spearman von Driver, Cornelius

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Effect of vertical-tail modifications on the static stability characteristics at mach number of 2.2 of a supersonic vtol airplane model having a broad fuselage and small delta wings / by Ross B. Robinson and M. Leroy Spearman von Robinson, Ross B

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Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 / by Cornelius Driver and M. Leroy Spearman von Driver, Cornelius

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Some effects of interference flowfields on supersonic configurations von Spearman, M. Leroy

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A lighter-than-air system enhanced with kinetic lift von Spearman, M Leroy

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Innovative Concept for a Heavy-Load Aircraft Utilizing a Two-Dimensional Wing von Spearman, M. Leroy

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Innovation in Aerodynamic Design Features of Soviet Missiles von Spearman, M. Leroy

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Longitudinal aerodynamic characteristics at Mach Numbers from 1.60 to 2.86 for a spanmissile with three wing planforms / M Leroy Spearman and Wallace C Sawyer von Spearman, M. Leroy

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Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 / by M. Leroy Spearman von Spearman, M. Leroy

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Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 / by M. Leroy Spearman and Arthur Henderson, Jr von Spearman, M. Leroy

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Stability and control characteristics at a mach number of 1.89 of a lightweight glider reentry configuration / by Ross B. Robinson and M. Leroy Spearman von Robinson, Ross B

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Effects of forebody length on the stability and control characteristics at a Mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing / by M. Leroy Spearman and Cornelius Driver von Spearman, M. Leroy

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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels / by M. Leroy Spearman and Gerald V. Foster von Spearman, M. Leroy

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Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° / by M. Leroy Spearman and Gerald V. Foster von Spearman, M. Leroy

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Wind-tunnel investigation of control-surface characteristics. XXIII, a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil / by M. Leroy Spearman von Spearman, M. Leroy

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Investigation of the aerodynamic characteristics in pitch and sideslip of a 45° swept-wing airplane configuration with various vertical locations of the wing and horizontal tail. Static lateral and directional stability ; Mach numbers of 1.41 and 2.01 / M. Leroy Spearman and Ross B. Robinson von Spearman, M. Leroy

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Lessons Learned in the High-Speed Aerodynamic Research Programs of the NACA/NASA von Spearman, M. Leroy

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