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1.
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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 | Driver,Cornelius. Material type:  Book Description: 28.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).
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2.
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NASA Memo [10-2-58L]
: AERODYNAMIC CHARACTERISTICS FOR COMBINED ANGLES OF ATTACK AND SIDESLIP OF A LOW-ASPECT-RATIO CRUCIFORM-WING MISSILE CONFIGURATION EMPLOYING VARIOUS CANARD AND TRAILING-EDGE FLAP CONTROLS AT A NO.2.01
by Robinson, Ross B | Spearman, M. Leroy. Description: 71p.Publisher: Washington National Aeronautics and Space Administration 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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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 | Spearman,M Leroy. Material type: Book Description: 27.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-441] (1).
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4.
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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 | Collins,Ida K. Material type: Book Description: 40.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7069] (1).
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5.
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SOME EFFECTS OF EXTERNAL STORES ON THE STATIC STABILITY OF FIGHTER AIRPLANES.
by Spearman,M Leroy. Material type: Book Description: 34.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6775] (1).
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6.
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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 | Spearman,M Leroy. Material type: Book Description: 17.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-519] (1).
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7.
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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 | Driver,Cornelius. Material type: Book Description: 30.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1263] (1).
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8.
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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. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 40p.Publisher: Washington, D.C. Nasa 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-839] (1).
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