PKK Library Search for 'su:{Stability} and se:NASA Technical Note'

NASA Technical Note [NASA TN D-4680]: Experimental investigation of the use of soft side legs to improve touchdown stability of legged landing vehicles

Washington NASA 1968 . 21p , Bound together NASA TN D-4671 to 4680 | Bound vol. Acc. No. 86062 contains Acc. No. TR10091 to TR10099

Place Hold on NASA Technical Note [NASA TN D-4680]: Experimental investigation of the use of soft side legs to improve touchdown stability of legged landing vehicles

NASA Technical Note: CALCULATED AND FLIGHT-MEASURED HANDLING-QUALITIES FACTORS OF THREE SUBSONIC JET TRANSPORTS

By McNeill, Walter E. Washington, D.C. NASA 1968 . 30p. , Technical Note D-4831-4840 | Bound Vol. No.101114 contents TR7567-7575

Place Hold on NASA Technical Note: CALCULATED AND FLIGHT-MEASURED HANDLING-QUALITIES FACTORS OF THREE SUBSONIC JET TRANSPORTS

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

Washington NASA 1961 . 70p , Bound together NASA TN D-441 to 450 | Bound vol. Acc. No. 63667 contains Acc. No. TR10185 to TR10193

Place Hold on 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

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

Washington NASA 1961 . 98p , Bound together NASA TN D-441 to 450 | Bound vol. Acc. No. 63667 contains Acc. No. TR10185 to TR10193

Place Hold on 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

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

Washington NASA 1970 . 35p , Bound together NASA TN D-5861 to 5870 | Bound vol. Acc. No. 101205 contains Acc. No. TR9523 to TR9531

Place Hold on 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

NASA Technical Note [NASA TN D-5870]: Steady-state and stability analysis of externally pressurized gas-lubricated journal bearings with herringbone grooves

Washington NASA 1970 . 40p , Bound together NASA TN D-5861 to 5870 | Bound vol. Acc. No. 101205 contains Acc. No. TR9523 to TR9531

Place Hold on NASA Technical Note [NASA TN D-5870]: Steady-state and stability analysis of externally pressurized gas-lubricated journal bearings with herringbone grooves

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

Washington NASA 1960 . 14p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on 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

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.. Washington, D. C. National Aeronautics and Space Administration 1961 . 78p , Bound vol. contains NASA TM X 350-396

Place Hold on 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]

NASA Technical Note [D-3191-3200]

Washington NASA 1966 , NASA TN D-3191: Payload optimization of multistage launch vehicle/ by Fred Teren and Omer F. Spurlock | NASA TN D-3192: Wind-tunnel investigation of longitudinal aerodynamics characteristics of a powered four-duct-propeller VTOL model in transition/ Kenneth P. Spreemann | NASA TN D-3193: Experimental stability and drag of a pointed and a blunted 30 degree half-angle cone at mach numbers from 11.5 to 34 in air/ by Peter F. Intrieri | NASA TN D-3194: Manned Mars landing missions using electric propulsion/ by John S. MacKay, Charles L. Zola, Leonard G. Rossa, Laurence H. Fishbach, William C. Strack, and Frank J. Hrach | NASA TN D-3195: Possible occurrence of boundary shock waves/ by E. Dale Martin | NASA TN D-3196: Effect of cold reduction and thermal treatment on tensile properties of a nickel - 2 percent beryllium alloy at cryogenic temperatures / Thomas W. Orange | NASA TN D-3197: Radiant heating of a seeded gas in a coaxial-flow gaseous reactor/ by Charles C. Masser | NASA TN D-3198: Dynamic instability of undamped bellows face seals in cryogenic liquid/ by John C. Hudelson | NASA TN D-3199: Behavior of a single-turn magnetic coil under dynamic load conditions/ by M.D. Williams and G. K. Oertel | NASA TN D-3200: Investigation of the use of Penetrometers to determine the capability of dust materials to support bearing loads/ by Brantley R. Hanks and John Locke McCarty

Place Hold on NASA Technical Note [D-3191-3200]

NASA Technical Note: Longitudinal stability and control derivatives of a Jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation

By Steinmetz, George G.. Washington, D. C. NASA 1962 . 43p. , Technical Note D-6532-6549 Bound Vol. No.101250 contents TR8009-8014

Place Hold on NASA Technical Note: Longitudinal stability and control derivatives of a Jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation