PKK Library Search for 'au:"Spearman,M Leroy"'

EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01

By Spearman,M Leroy. Nasa, Washington, D.C. 1959 . 28 , Bound With Nasa Memo 4-1-59l-4-19-59l

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NASA Memo [10-2-58L]

By Robinson, Ross B.. Washington National Aeronautics and Space Administration 1958 . 71p , NASA Memorandum 10-1-58L-10-17-58L Bound Vol. No.102461; Contents: TR-8572-8580

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STABILITY AND CONTRL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

By Driver,Cornelius. Nasa, Washington, D.C. 1961 . 27 , Bound With Nasa Tm X-416-40,448-79 Lack No.418-22,24,26,28-29,32,34-36,38,42-47,50-58,60-66,69-78

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AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING CRUISE MISSILE AT MACH NUMBERS FROM 0.50 TO 2.86

By Spearman,M Leroy. Nasa, Washington, D.C. 1972 . 40 , Bound With Nasa Tn D-7060-7068

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SOME EFFECTS OF EXTERNAL STORES ON THE STATIC STABILITY OF FIGHTER AIRPLANES.

By Spearman,M Leroy. Nasa, Washington, D.C. 1972 . 34 , Bound With Nasa Tn D -6770-74,6776-79.Lack No-6777.

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EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

By Robinson,Ross B. Nasa, Washington, D.C. 1961 . 17 , Bound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

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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 Spearman,M Leroy. Nasa, Washington, D.C. 1962 . 30 , Bound With Nasa Tn D-1261-1262,1264-1270

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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 [NASA TN D-839]

By Spearman, M. Leroy. Washington, D.C. Nasa 1961 . 40p

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