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21.
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Measurement of heat transfer, recovery temperature and pressure destribution on delta wings at M=3 Description: 48p.Publisher: Stockholm 1963Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 629.505 Sw31m] (1).
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22.
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Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles
by Reed, Wilmer H | NASA Washington. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D 1821-1830] (1).
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23.
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Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820
by NASA : National Aeronautics and Space Administration. Material type: Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington NASA 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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24.
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Technical reports no. TN D-1796 to D-1800 Material type: Book Description: various pages.Publisher: Washington, DC National Aeronautics and Space Administration [NASA] 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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25.
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A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogy[NASA TN D-3767]
by Polhamus,Edward.C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 15p.Publisher: Washington,D.C. National Aeronautics And Space Administration 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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26.
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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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27.
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Numerical solution of supersonic and hypersonic viscous flow fields around thin planar delta wings
by Bluford, G. S. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 212p.Publisher: USA Air Force Institute of Technology, Air University 1978Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: AFIT ADA056513] (1).
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28.
|
The experimental and calculated characteristics of 22 tapered wings [Report No.627]
by Anderson,Raymond F. 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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29.
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Aerodynamic center considerations of wings and wing body combinations [NASA TN D-3581]
by Lamar, John E | Alford, William J. Material type: Book; Format:
print
; Literary form:
not fiction
Publisher: Washington National Aeronautics and Space Administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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30.
|
Relative loading on biplane wings [Report no. 458]
by Diehl, Walter S. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 17p.Publisher: Washington, D. C. National Advisory Committee for Aeronautics 1933Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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31.
|
Investigation at mach numbers of .60 to 3.50 of blended wing body combinationswith cambered and twisted wings with diamond, delta and arrow plan forms [NASA TM X-390]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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