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1.
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A THEORETICAL INVESTIGATION OF THE DRAG OF GENERALIZED AIRCRAFT CONFIGURATIONS IN SUPERSONIC FLOW.
by Graham,E W,Rstron,P A | Licher,R M. Material type:  Book Description: 108.Publisher: National Advisory Committee For Aeronautics, Washington,D.C. 1957Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NACA 1421] (1).
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2.
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ON LANDING GEAR STRESSES
by Gentric,A. Material type: Book Description: 45.Publisher: National Advisory Committee For Aeronautics, Washington,D.C. 1956Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NACA TM-1422] (1).
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3.
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ON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE
by Corcos,G M | Liepmann,H W. Material type: Book Description: 43.Publisher: National Advisory Committee For Aeronautics, Washington,D.C. 1956Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NACA TM-1420] (1).
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4.
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Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
by Stokes, Fred H | Matthews, J. T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Advisory Committee for Aeronautics 1953Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NACA TN-2882] (1).
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5.
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Smoke of nozzle secondary flows in a low speed turbine [TN 3260]
by Kofskey, Milton G | Allen, Hubert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 24p.Publisher: Washington National Advisory Committee for Aeronautics 1954Availability: No items available
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6.
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Airfoil section characterstics as applied to the prediction of air forces and their distribution on wings[R.No.631]
by Jacobs,Eastman N | Rhode,R.V. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 29p.Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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The crinkling strength and the bending strength of round aircraft tubing[R.No632]. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 15p.Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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Pressure distribution over an N.A.C.A.23012 airfoil with a slotted and a plan flap
by Wenzinger,Carl J | Delano,James B. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 32p.Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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9.
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Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]
by Allen,H.Julian. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 16p.Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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10.
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Theoretical stability and control characteristics of wings with various amounts of taper and twist [R.No.635]
by Pearson,Henry A | Jones,Robert T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 17p.Publisher: Washington,D.C National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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11.
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Approximate stress analysis of multi-stringer beams with shear deformation of the flanges[R.No.636]
by Kuhn,Paul. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 21p.Publisher: Washington,D.C. National advisory committee for aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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12.
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Determination of boundary layer transition on three symmetrical airfoils in the N.A.C.A. full scale wind tunnel [R. No.637]
by Silverstein, Abe | Becker, John V. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 15p.Publisher: Washington,D.C. National Advisory Committee for Aeronautics 1939Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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13.
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The infulence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts [R.No. 638]
by Jones, Robert T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 10p.Publisher: Washington, D.C. National Advisory Committee for Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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14.
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The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range[R.No.639]
by Biermann,David | Hartman,Edwin P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 29p.Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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15.
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The aerodynamic characteristics of full-scale propellers having 2,3, and 4 blabes of clark Y and R.A.F.6 airfoil sections[R.No.640]
by Hartman,Edwin P | Biermann,David. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 23p.Publisher: Washington.D.C. National Advisory Committee For Aeronautics 1938Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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16.
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Measurement and power spectra of runway roughness at airports in countries of the north atlantic treaty organization [Technical Note-4303]
by Thompson,Wilbur E. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 85p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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17.
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Matrix method for obraining spanwise moments and deflections of torsionally rigis rotor blades with arbitrary loadings [Technical Note 4304]
by Mayo, Alton P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 51p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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18.
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Wind tunnel investigation of effects ofspoilerocation, spoiler size, and fuselage nose shape on directional charecteristics of a model of a model of a tandem-rotor helicopter fuselage [NACA TN-4305]
by Williams, James L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 44p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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Temperature and thermal stress distributions in some structural elements heated at a constant rate [NACA TN-4306]
by Brooks, William A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington National Advisory Committe for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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20.
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Transient temperature distribution in two component semi infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat transfer coefficient [Technical Note 4308]
by Trimpi, Robert L | Jones, Robert A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 83p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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