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1.
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NASA Technical Note [NASA TN D-4680]: Experimental investigation of the use of soft side legs to improve touchdown stability of legged landing vehicles
by Washington. National Aeronautics and Space Administration (NASA) | Robert W. Herr. Material type:  Book Description: 21p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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2.
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NASA Technical Note: CALCULATED AND FLIGHT-MEASURED HANDLING-QUALITIES FACTORS OF THREE SUBSONIC JET TRANSPORTS
by McNeill, Walter E. Material type: Book Description: 30p.Publisher: Washington, D.C. NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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NASA Technical Note [NASA TN D-444]: Lateral stability and control characteristics of a four-propeller deflected-slipstream VTOL model including the effects of ground proximity
by Washington. National Aeronautics and Space Administration (NASA) | Kuhn, Richard E | Grunwald, Kalman J. Material type: Book Description: 70p.Publisher: Washington NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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NASA Technical Note [NASA TN D-445]: Investigation of longitudinal and lateral stability characteristics of a six-propeller deflected-slipstream VTOL model with boundary-layer control including effects of ground proximity
by Washington. National Aeronautics and Space Administration (NASA) | Grunwald, Kalman J. Material type: Book Description: 98p.Publisher: Washington NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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NASA Technical Note [NASA TN D-5862]: Simulator study of the instrument landing approach of a heavy subsonic jet transport with an external-flow jet-flap system used for additional lift
by Washington. National Aeronautics and Space Administration (NASA) | Grantham, William D | Deal, Perry L | Sommer, Robert W. Material type: Book Description: 35p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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6.
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NASA Technical Note [NASA TN D-5870]: Steady-state and stability analysis of externally pressurized gas-lubricated journal bearings with herringbone grooves
by Washington. National Aeronautics and Space Administration (NASA) | Fleming, David P. Material type: Book Description: 40p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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NASA Memorandum [NASA MEMO 4-20-59A]: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22- lateral-directional characteristics of an unswept wing and canard
by Washington. National Aeronautics and Space Administration (NASA) | Peterson, Victor L. Material type: Book Description: 32p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0
by Washington. National Aeronautics and Space Administration (NASA) | Osborne, Robert S | Kelly, Thomas C. Material type: Book Description: 14p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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9.
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Description of an analog computer approach to v/stol simulation employing a variable stability helicopter [NASA TN D-1970]
by Garren, John F | Kelly, James R. Material type: Book Description: 13p.Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1970] (1).
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10.
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Input design for identification of aircraft stability and control derivatives [NASA CR -2493]
by Gupta, Narendra K | Hall, W. Earl. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 133p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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11.
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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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12.
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Aerodynamic stability characteristics of the apollo launch escape vehicle (LEV) with canard surfaces deployed [NASA TN D-4280]
by Moseley, William C | Redd, Bass. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 98p.Publisher: Washington, D.C. National Aeronautics and Space Administration (NASA) 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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13.
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Elastic stability of laminated, flat and cured, long rectangular plates subjected to combined inplane loads
by Viswanathan, A.V | Tamekuni, M | Baker, L.L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: iii,65p.Publisher: Washington,D.C. National Aeronautics and Space Administration 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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14.
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Determination of lateral stability characteristics from free flight model tests, with experimental results on the effects of wing vertical position and dihedral at transonic speeds [NASA TR-65]
by Gilles, Clarence L | Mitchell, Jesse L | D'Aiutolo, Charles T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 35p.Publisher: Washington,D.C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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15.
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Investigation of the static stability characteristics of two stages of a three-stage missile at a Mach number of 4.00 [NASA TN D-651--TN D-660]]
by Carraway, Ausley B | Edwards, Frederick G | Keating, Jean C. Description: 18p.Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-651] (1).
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16.
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Static stability charectristics at mach numbers from 1.90 to 4.63 of a 76 degree swept arrow wing model with variations in horizontal tail height wing height and dihedral [NASA TN D-4076]
by Fuller, Dennis E. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 115p.Publisher: Washington, D. C. National Aeronautics and Space Administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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17.
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Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives [NASA CR-2200]
by Stepner, David E | Mehra, Raman K. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 193p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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18.
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Stability and control characterstics of a small scale model of an aerial vehicle supported by two ducted fans [NASA TN D-920]
by Parlett, Lysle P. Material type: Book Description: 22p.Publisher: Washingtom National aeronautics and space administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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Dynamic stability and dispersion of a project mercury test capsule upon entering the atmosphere , with effects of roll rate centre of gravity diplacement, and threshold of a rate reaction control system [NASA TM X-350]
by Jaquet, Byron M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 78p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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20.
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NASA Technical Note [D-3191-3200]
by Teren, Fred | Spurlock, Omer F | Spreemann, Kenneth P | Intrieri, Peter F | MacKay, John S | Hrach, Frank J | Strack, William C | Fishbach, Laurence H | Rossa, Leonard G. Zola, Charles L | Martin, E. Dale | Orange, Thomas W | Masser, Charles C | Williams, M.D | Oertel, G. K | Hudelson, John C | Hanks, Brantley R | McCarty, John Locke. Material type: Book Publisher: Washington NASA 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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