|
21.
|
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).
|
|
22.
|
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).
|
|
23.
|
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).
|
|
24.
|
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).
|
|
25.
|
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).
|
|
26.
|
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).
|
|
27.
|
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).
|
|
28.
|
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).
|
|
29.
|
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).
|
|
30.
|
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).
|
|
31.
|
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).
|
|
32.
|
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).
|
|
33.
|
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).
|
|
34.
|
Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept wing bomber in rough air [NACA TN-4307]
by Engel, Jerome N. Material type: Book; Format:
print
; Literary form:
not fiction
Publisher: Washington, D. C. National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
35.
|
Use of shotr flat vanes for producing efficient wide angle two-dimensional subsonic diffusers [NACA TN-4309]
by Cochran, D. L | Kline, S. J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 135p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
36.
|
A method for evaluating the effects of drag and inlet presuure recovery on propulsion system performance [NACA Note-3261]
by Kremzier, Emil J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 21p.Publisher: Washington , D. C. National Advisory Committee for Aeronautics 1954Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
37.
|
A method for evaluating the effects of drag and inlet pressure recovery on propulsion system performance [ Technical Note 3261 ]
by Kremzier, Email J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 21p.Publisher: Washington National Advisory committee for Aeronautics 1954Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
38.
|
Starting and operating limits of two supersonic wind tunnels utilizing auxiliary air injection downstream of the test section [ Technical Note 3262 ]
by Hunczak, Henry R | Rousso, Morris D. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 26p.Publisher: Washington National Advisory Committee for Aeronautics 1954Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
39.
|
Lift and moment equations for oscillating airfouls in an infinite unstaggered cascade [TN-3263]
by Mendelson, Alexander | Carroll, Robert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 46p.Publisher: Washington National Advisory Committee for Aeronautics 1954Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
40.
|
Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients [Technical Note 3264]
by Sandborn, Virgil A | Slogar, Raymond J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 79p.Publisher: Washington National Advisory Committee for Aeronautics 1955Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|