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1.
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Wind tunnel investigation of the formation of a trailing vortex
by Francis, Michael Skok. Material type: Book; Format:
print
; Literary form:
not fiction
Description: xviii, 199p.Publisher: Michigan University Microfilms International 1983Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 629.13432 F847w] (1).
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2.
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COMPARISON OF PREDICTIONS OBTAINED FROM WIND TUNNEL TESTS AND THE RESULTS FROM CRUISING FLIGHT (AIRBUS AND CONCORD)
by Berger,J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69.Publisher: Nasa, Washington, D.C. 1979Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 629.13452 B453C] (1).
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3.
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NASA Technical Note [NASA TN D-5936]: Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings
by Washington. National Aeronautics and Space Administration (NASA) | Naeseth, Rodger L. Material type: Book Description: 102p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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NASA Technical Note [NASA TN D-4672]: Wind-tunnel investigation of the static aerodynamic characteristics of a multilobe gliding parachute
by Washington. National Aeronautics and Space Administration (NASA) | Ware, George M | Libbey Charles E. Material type: Book Description: 21p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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NASA Technical Note [NASA TN D-4678]: Wind-tunnel calibration of a 40 degree conical pressure probe at mach numbers from 3.5 to 7.4
by Washington. National Aeronautics and Space Administration (NASA) | Burcham, Frank W. Material type: Book Description: 24p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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6.
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NASA Technical Note [NASA TN D-3447]: Measured and calculated flow conditions on the forward fuselage of the X-15 airplane and model at mach numbers from 3.0 to 8.0
by Washington. National Aeronautics and Space Administration (NASA) | Palitz, Murray. Material type: Book Description: 44p.Publisher: Washington NASA 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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Wind-tunnel investigation of an stol aircraft configuration equipped with an external-flow jwt flap [NASA TN D-5364]
:
by Parlett, Lysle P | Shivers, James P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 85p.Publisher: Washington, D.C. Nasa 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories
by Washington. National Aeronautics and Space Administration (NASA) | Lockwood, Vernard E | Phillips, W. Pelham. Material type: Book Description: 38p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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9.
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NASA Technical Note: INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC TRANSPORT MODEL AT MACH NUMBERS TO 6
by Ellison, James C. Material type: Book Description: 79p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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10.
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NASA Technical Note : STABILITY AND CONTROL CHARACTERISTICS OF A 0.0667-SCALE MODEL OF THE FINAL VERSION OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE (CONFIGURATION 3) AT TRANSONIC SPEEDS
by Osborne, Robert S. Material type: Book Description: 102p.Publisher: Washington, D.C. NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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11.
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Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine low-wing airplane [NASA TN D-5857]
by Shivers, James P | Fink, Marvin P | Ware, George M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 63p.Publisher: Washington, D.C. Nasa 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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12.
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A WIND-TUNNEL INVESTIGATION OF A TRANSONIC-TRANSPORT CONFIGURATION UTILIZING DRAG-REDUCING DEVICES AT MACH NUMBERS FROM 0.20 TO 1.03 [NASA TN D-636]
by Loving, Donald L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 117p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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13.
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Wind-tunnel investigation of a tilt-wing vtol-airplane with articulated rotors. [NASA TN D-2538]
by Weilberg, James A | Giulianetti, Demo J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 55p.Publisher: Washington, D.C. Nasa 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2538] (1).
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14.
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NASA Technical Note [NASA TN D-2935]: Study of gas injection in the boundary layer of a hypersonic wind tunnel to extend the useful operating range
by Washington. National Aeronautics and Space Administration (NASA) | McDevitt, John B. Material type: Book Description: 33p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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15.
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WIND-TUNNEL MEASUREMENTS OF AERODYNAMIC DAMPING DERIVATIVES OF LAUNCH VEHICLE VBRATING IN FREE-FREE BENDING MODES AT MACH NUMBERS FROM 0.70 TO 2.87 AND COMPARISONS WITH THEORY. [NASA TN D-1391]
by Hanson, Perry W.[ | Perry W. Hanson and Robert V. Doggett. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Nasa Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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16.
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Transonic wind tunnel testing
by Goethert, Bernhard H | Nelson, Wilbur C.[Ed.] | Advisory Group of Aeronautical Research and Development (AGARD) North Atlantic Treaty Organization (NATO). Material type: Book Description: xvii, 397p.Publisher: London Pergamon Press 1961Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 629.505 Ad9ag] (1).
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17.
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WIND TUNNEL MODELING FOR CIVIL ENGINEERING APPLICATIONS
by Reinhold, Timothy A | . Description: xi.Publisher: Cambridge University 1982Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 624.17500287 In8c] (1).
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18.
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A wind tunnel investigation of pressure flactations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane [NASA TN D-1359]
by Mckee, John W. and Thomas, A.Byrdsong | Thomas, A.Byrdsong. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 29p.Publisher: Washingto, D. C. NASA JUNE 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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The boundaary-Layer transition characteriasics of two bodies of revolution, And an unswept wing in a Low-Turbulence wind tunnel [NASA TN D-309] -
by Boltz, Frederick W., Kenyon, George C. and Allen, Clyde Q | Allen, Clyde Q | Kenyon, George C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 45p.Publisher: Washington, D. C. NASA April 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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20.
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Large scale wind tunnel tests of a circulra form aircraft with a peripheral jet forLift [NASA TN D-1432]
by Greif, Richard K | Tolhurst, William H. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 97p.Publisher: Washington, D. C. NASA Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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