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NASA Technical Note [NASA TN D-3442]: Low-subsonic wind-tunnel and free-flight drop-test investigation of a paraglider configuration having large tapered leading edges and keel
by Washington. National Aeronautics and Space Administration (NASA) | Croom, Delwin R | Fournier, Paul G. Material type:  Book Description: 32p.Publisher: Washington NASA 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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2.
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LOW-SPEED WIND-TUNNEL INVESTIGATION OF ALL-FLEXIBLE TWIN-KEEL TENSION-STRUCTURE PARAWINGS
by Fournier,Paul G. Material type: Book Description: 84.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5965 -] (1).
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3.
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WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE
by Fournier,Paul G. Material type: Book Description: 21.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).
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4.
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LOW SUBSONIC PRESSURE DISTRIBUTIONS ON THREE RIGID WINGS SIMULATING PARAGLIDERS WITH VARIED CANOPY CURVATURE AND LEADING-EDGE SWEEP
by Fournier,Paul G, Bell,Ann. Material type: Book Description: 51.Publisher: Nasa,Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-983 -] (1).
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5.
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WIND-TUNNEL STUDIES OF EFFECTS OF CONSTRUCTION METHODS, DESIGN DETAILS, AND CANOPY SLOTS ON THE AERODYNAMIC CHARACTERISTICS OF SMALL-SCALE ALL-FLEXIBLE PARAWINGS
by Fournier,Paul G | Sleeman,William C. Material type: Book Description: 91.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5974] (1).
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6.
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LOW-SPEED WIND-TUNNEL INVESTIGATION OF TENSION-STRUCTURE PARAWINGES.
by Naeseth,Rodger L | Fournier,Paul G. Material type: Book Description: 189.Publisher: Nasa, Washington, D.C. 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-3940] (1).
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7.
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PRESSURE DISTRIBUTIONS ON THREE RIGID WINGS SIMULATING PARAWINGS WITH VARIED CANOPY CURVATURE AND LEADING-EDGE SWEEP AT MACH NUMBERS FROM 2.29 TO 4.65
by Fournier,Paul G. Material type: Book Description: 113.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1618] (1).
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8.
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AERODYNAMIC CHARACTERISTICS AT LOW SPEED OF A REENTRY6 CONFIGURATION HAVING RIGID RESTRACTABLE CONICAL LIFTING SURFACES
by Fournier,Paul G. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-622] (1).
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9.
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LOW -SPEED INVESTIGATION OF STATIC LONGITUINAL AND LATERAL STABILITY CHRACTERISTICS OF AN AIRPLANE CONFIGURATION WITH A HIGHLY TAPERED WING AND WITH SEVRAL BODY AND TAIL ARRANGMENTS.
by Fournier,Paul G. Material type: Book Description: 46.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-217] (1).
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10.
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EFFECT OF HALL DIHEDRAL ON LATERAL CONTROL EFFECTIVENESS AT HIGH SUBSONIC SPEEDS OF DIFFERENTIALLY DEFLECTED HORIZONTAL-TAIL SURFACES ON A CONFIGURATION HAVING A THIN HIGHLY TAPERED WING
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by FOURNIER,PAUL G. Material type: Book; Format:
print
; Nature of contents:  Description: ,50.Publisher: NASA, WASHINGTON, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 12-1-58L - ] (1).
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