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1.
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HOVERING AND TRANSITION FLIGHT TESTS OF A 1/5-SCALE MODEL OF JET-POWERED VERTICAL-ATTITUDE VTOL RESEARCH AIRPLANE.
by Smith,Charles C. Material type:  Book Description: 30.Publisher: Nasa, Washington, D.C. 1958Availability: No items available Damaged (1).
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2.
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WIND-TUNNEL INVESTIGATION OF A JET TRANSPORT AIRPLANE CONFIGURATION WITH HIGH THRUST-WEIGHT RATIO AND AN EXTERNAL-FLOW JET FLAP
by Parlett,Lysle P,Freeman,Delma C | Smith,Charles C. Material type: Book Description: 74.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6058] (1).
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3.
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A WIND-TUNNEL INVESTIGATION OF STATIC LONGITUDINAL AND LATERAL CHARACTERISTICS OF A FULL-SCALE MOCK UP OF A LIGHT TWIN-ENGINE AIRPLANE
by Fink,Marvin P,Shivers,James P | Smith,Charles C. Material type: Book Description: 268.Publisher: Nasa, Washington, D.C. 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6238] (1).
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4.
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HOVERING AND TRANSITION FLIGHT TESTS OF A 1/5-SCALE MODEL OF A JET-POWERED VERTICAL-ATTITUDE VTOL RESERACH AIRPLANE.
by Smith,Charles C. Material type: Book Description: 30.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-404] (1).
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5.
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GENERALIZED HOT-GAS INGESTION INVESTIGATION OF LARGE-SCALE JET VTOL FIGHTER-TYPE MODELS
by Mclemore,H Clyde,Smith,Charles C | Hemeter,Patricia G. Material type: Book Description: 152.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5581] (1).
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6.
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LOW-SPEED MEASUREMENTS OF STATIC AND OSCILLATORY LATERAL STABILITY DERIVATIVES OF A 1/5-SCALE MODEL OF A JET-POWERD VERTICAL-ATTITUDE VTOL RESEARCH AIRPLANE
by Shanks,Robert E | Smith,Charles C. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-433] (1).
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7.
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NASA TN [D-5481]
: PRESSURE DISTRIBUTION OF A LARGE SEMISPAN TILTING WING WITH 0.4-DIAMETER-CHORD, SINGLE-SLOTTED FLAP, AND A SINGLE PROPELLER 0.22 CHORD BELOW WING.
by Fink, Marvin P | Smith, Charles C. Description: 379p.Publisher: Washington National Aeronautics and Space Administration 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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Wind tunnel investigation of the flight characteristics of a model of an aspect ratioo 6 conical parawing utility vehicle (NASA TN D-3673)
by Smith, Charles C | Ware, George M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 39P.Publisher: Washington,D.C. National Aeronautics and Space Administration 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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