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1.
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FLOW FIELD SURVEY AND DECELERATOR DRAG CHARACTERISTICS IN THE WAKE OF A MODEL OF THE X-15 AIRPLANE AT MACH 2.0 AND 4.65
by Campbell,James F. Material type:  Book Description: 35.Publisher: Nasa, Washington, D.C. 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-3285 -] (1).
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2.
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Experimental flow properties in the wake of a 120 degree cone at mach number 2.20 [NASA TN D-5365]
by Campbell, James F | Grow, Josephine W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 54p.Publisher: Washington, D.C. Nasa 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL HIGH-DRAG BODIES AT MACH NUMBERS FROM 1.50 TO 4.63
by Campbell,James F. Material type: Book Description: 32.Publisher: Nasa, Washington, D.C. 1967Availability: No items available Damaged (1).
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4.
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SUPERSONIC AERODYNAMIC CHARACTERISTICS AND SHOCKS STANDOFF DISTANCES FOR LARGE-ANGLE CONES WITH AND WITHOUT CYLINDRICAL AFTERBODIES
by Campbell,James F. Material type: Book Description: 96.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5334] (1).
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5.
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Evaluation of flow properties behind 120 degree and 140 degree included angle cones and a viking 75 entry vehicle at mach numbers from 1.60 to 3.95
by Brown, Clarence A | Campbell, James F. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 100p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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6.
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BOUNDARY-LAYER TRANSITION STUDY OF SEVERAL PLINTED BODIES OF REVOLUTION AT SUPERSONIC SPEEDS
by Cassels,William A | Campbell,James F. Material type: Book Description: 67.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6063] (1).
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7.
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PRESSURE DISTRIBUTIONS ON 140(DEGRE),160(DEGRE) AND 180(DEGRE) CONES AT MACH NUMBERS FROM 2.30 TO 4.63 AND ANGLES OF ATTACK FROM 0 (DEGRE) TO 20(DEGRE)
by Campbell,James F | Tudor,Dorothy H. Material type: Book Description: 147.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5204] (1).
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8.
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SUPERSONIC AERODYNAMICS OF LARGE-ANGLE CONES
by Campbell,James F | Howell,Dorothy T. Material type: Book Description: 71.Publisher: Nasa, Washington, D.C. 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4719] (1).
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