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21.
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A wind tunnel investigation at a mach number of 2.01 of the sonic boom characteristics of three wing body combinations differing in wing longitudinal location ( NASA TN D-1384)
by Morris, Odell A. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: 17p.Publisher: Washington National Aeronautics and Space Administration 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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22.
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Theoretical determination of the boundary and distortion of the geomagnetic field in a steady solar wing [ NASA TR R-178]
by Briggs, Benjamin R | Spreiter, John R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 17p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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23.
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An evaluation of effects of flexibility on wing strains in rough air for a large swept wing airplace by means of experimentally determined frequency reponse funtions with an assessment of random process technuques employed [ NASA TR R-70]
by Coleman, Thomas L | Press, Harry | Meadows, May T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 33p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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24.
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An experimental investigation of a triangular wing of aspect ration 2 and a body warped to be trimmed at M=224 [Gaynor J. Adoms and John W. Boyd]
by Adams, Gaynor J | Boyd, John W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 38p.Publisher: Washington National Aeronautics and Space Administration 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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25.
|
Computer programs for calculating the static longitudinal aerodynamic characteristics of wing body tail configurations [NASA CR-2474]
by Micbael,R | Goodwin,Frederick K | Dillenius,Marnix F.E | Kline,David M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 218p.Publisher: Washington,D.C. National Aeronautics and Space Administration 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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26.
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Computer programs for calculating the static longitudinal aerodynamic characteristics of wing body tail configurations [NASA CR-2474]
by Micbael,R | Goodwin,Frederick K | Dillenius,Marnix F.E | Kline,David M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 218p.Publisher: Washington,D.C. National Aeronautics and Space Administration 1975Availability: No items available
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27.
|
General potential theory of arbitrary wing sections [Report no. 452]
by Theodorsen, T | Garrick, I. E. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 35p.Publisher: Washington, D. C. National Advisory Committee for Aeronautics 1940Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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28.
|
Extraction from flight data of lateral aerodynamic coefficients for F-8 aircraft with supercritical wing [NASA TN D-7749]
by Williams, James L | Suit, William T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 35p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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29.
|
The effects of wing plan from on the the static longitudinal aerodynamic characteristics of a flat-top hypersonicaircraft at mach numbers from 0.6 to 1.4 [NASA TM X-364]
by Treon, Stuart L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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30.
|
Evaluation of blended wing body combinations with curved plan forms at mach numbersn uoto 3.50 [NASA TM X-379]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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31.
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Flight-Test investigation of ailerons as a source of yaw control on the VZ-2 tilt-wing aircraft
: TN D-1375
by Pegg, Robert J. Material type: Book Description: 24p.Publisher: Washington NASA 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: TRNASATND-1375] (1).
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