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21. NASA Memorandum [NASA MEMO 4-21-59A]: Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody

by Washington. National Aeronautics and Space Administration (NASA) | Boyd, John W | Menees, Gene P.

Material type: book Book Description: 39p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

22. NASA Memorandum [NASA MEMO 4-26-59A]: Flight measurements of the effect of a controllable thrust reverser on the flight characteristics of a single-engine jet airplane

by Washington. National Aeronautics and Space Administration (NASA) | Anderson, Seth B | Cooper, George E | Faye, Alan E.

Material type: book Book Description: 45p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

23. NASA Memorandum [NASA MEMO 4-27-59A]: Lift-drag ratios for an arrow wing with bodies at mach number 3

by Washington. National Aeronautics and Space Administration (NASA) | Jorgensen, Leland H.

Material type: book Book Description: 32p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

24. NASA Memorandum [NASA MEMO 4-14-59A]: Sampled-data techniques applied to a digital controller for an altitude autopilot

by Washington. National Aeronautics and Space Administration (NASA) | Schmidt, Stanley F | Harper, Eleanor V.

Material type: book Book; Format: print ; Nature of contents: biography Description: 71p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

25. Estimation of directional stability derivatives at moderate angles and supersonic speeds

by Kattaari, George E.

Description: 71p.Publisher: Washington NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

26. NASA Memo [10-1-58L] : longitudinal and lateral stability and control characteristics of various combinations of the component parts of two canard airplane configurations at mach numbers of 1.41 and 2.01

by Driver, Cornelius.

Description: 104p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

27. NASA MEMO 3-3-59E : performance of two boron-modified S-816 alloys in a turbojet engine operated at 1650F

by Waters, William J | Signorelli, Robert A | Johnston, James R.

Description: 30p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

28. NASA MEMO 3-4-59E : effects of nose radius and extreme cooling on boundry layer transition for three smooth 15 cone cylinders in free flight at mach numbers to 8.50

by Krasnican, M.J | Rabb, L.

Description: 59p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

29. NASA MEMO 3-5-59E : stability of ceramics in hydrogen between 4000 and 4500F

by May, Charles E | Koneval, Donald | Fryburg, George C.

Description: 13p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

30. NASA MEMO 3-6-59E : preliminary study of a piston pump for cryogenic fluids

by Biermann, Arnold E | Kohl, Robert C.

Description: 27p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

31. NASA MEMO 3-9-59E : tensile properties of molybdenum and tungsten from 2500 to 3700F

by Robert W. Hall | Sikora, Paul F.

Description: 29p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

32. NASA MEMO 3-9-59E : optimization of parametric constants for creep-rupture data by means of least square

by Manson, S.S | Mendelson, A.

Description: 34p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

33. NASA MEMO 3-17-59E : analysis and evaluation of supersonic

by Roger, W. Luidens | Flaherty, Richard J.

Description: 55p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

34. NASA MEMO 3-18-59E : effect on inlet performance of a cowl visor an an internal contraction cowl for drag reduction at mach numbers 3.07 and 1.89

by Gertsma, Laurence W.

Description: 21p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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