PKK Library Search for 'su:{ Airplane }'

Airplane performance stability and control

By Perkins, Courtland D.. New York John Wiley & Sons 1949 . 493p.

Place Hold on Airplane performance stability and control

ANALYTICAL INVESTIGATION OF THE LANDING DYNAMICS OF A LARGE AIRPLANE WITH A LOAD-CONTROL SYSTEM IN THE MAIN LANDING GEAR

By Mcgehee,John R., Garden,Huey D.. Nasa,Washington, D.C. 1979 . 81

Place Hold on ANALYTICAL INVESTIGATION OF THE LANDING DYNAMICS OF A LARGE AIRPLANE WITH A LOAD-CONTROL SYSTEM IN THE MAIN LANDING GEAR

Determination of airplane model structure from flight data by using modified stepwise regression

By Klein, Vladislav. National Aeronautics And Space Administration 1981 . 46p.

Place Hold on Determination of airplane model structure from flight data by using modified stepwise regression

AVIATION DISASTERS

By Gero,David. Patrick Stephens Ltd., Somerset 1996 . 240 , Includes Bibliographical References 185260526X

Place Hold on AVIATION DISASTERS

DESIGN OF THE AEROPLANE

By Stinton,Darrol. Blackwell Science, Oxford 1983 . xxxiv,684 , Includes Bibliographical References And Index. 0632054018

Place Hold on DESIGN OF THE AEROPLANE

Introductrion to aircraft flight mechanics: performance, static stability, dynamic stability, and classical feedback control

By Yechout, Thomas R.. Restone, Virginia American Institute Of Aeronautics And Astronautics 2003 . xv, 634p.

Place Hold on Introductrion to aircraft flight mechanics: performance, static stability, dynamic stability, and classical feedback control

The great international paper airplane book

By Mander, Jerry. New York Simon And Schuster 1967 . 128p 0671289918

Place Hold on The great international paper airplane book

Landing impact studies of a 0.3 scale model air cushion landing system for a navy fighter airplane [NASA TN D-7875]

By Leland,Trafford J.W.. Washington, D.C. National Aeronautics And Space Administration 1975 . 33

Place Hold on Landing impact studies of a 0.3 scale model air cushion landing system for a navy fighter airplane [NASA TN D-7875]

NASA Technical Note: FLIGHT TESTS OF DIRECT LIFT CONTROL SYSTEM DURING APPROACH AND LANDING

By Stickle, Joseph W.. Washington, D.C. NASA 1968 . 44p. , Bound Volume No.101116 Contents TR 7622-7630 | Technical Note D-4851-4860

Place Hold on NASA Technical Note: FLIGHT TESTS OF DIRECT LIFT CONTROL SYSTEM DURING APPROACH AND LANDING

Use of multiple discrete wall jets for delaying boundary layer separation [NASA CR-2389]

By Mclean, J. D.. Washington, D.C. NASA 1974 . 74p

Place Hold on Use of multiple discrete wall jets for delaying boundary layer separation [NASA CR-2389]

Statistical analysis of landing-contact conditions for the xb-70 airplane [ NASA TN D-4007]

By Wilson, Ronald J.. Washington, D.C. Nasa 1967 . 27p

Place Hold on Statistical analysis of landing-contact conditions for the xb-70 airplane [ NASA TN D-4007]

NASA Technical Note [NASA TN D-5272]: An experimental and theoretical investigation of a symmetrical and a cambered delta wing configuration at mach numbers from 2.0 to 10.7

Washington NASA 1969 . 31p , Bound together NASA TN D-5271 to 5280 | Bound vol. Acc. No. 101151 contains Acc. No. TR7891 to TR7899

Place Hold on NASA Technical Note [NASA TN D-5272]: An experimental and theoretical investigation of a symmetrical and a cambered delta wing configuration at mach numbers from 2.0 to 10.7

NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories

Washington NASA 1968 . 38p , Bound together NASA TN D-4321 to 4330 | Bound vol. Acc. No. 86052 contains Acc. No. TR8602 to TR8610

Place Hold on NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories

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-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

FLIGHT INVESTIGATION OF STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-45]

By Tosti, L. P.. Washington, D.C. National Aeronautics and Space Administration 1960 . 25p , Bounds vol. contains TN D-41-45

Place Hold on FLIGHT INVESTIGATION OF STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-45]

NASA Technical Note [NASA TN D-1946]: Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle

Washington NASA 1963 . 72p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1946]: Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle

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

Nasa, Washington, D.C. 1959 . 32p , Bound together NASA MEMO 4-14-59A to 4-27-59A Lack No.4-16 to 4-17, 4-22 to 4-25 | Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615

Place Hold on 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

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

Washington NASA 1959 . 45p , Bound together NASA MEMO 4-14-59A to 4-27-59A Lack No.4-16 to 4-17, 4-22 to 4-25 | Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615

Place Hold on 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

EFFECTS OF AN IN-FLIGHT THRUST REVERSER ON THE STABILITY AND CONTROL CHARACTERISTICS OF A SINGLE-ENGINE FIGHTER AIRPLANE MODEL [NASA TN D-6886]

By Mercer, C. E.. Washington, D.C. National Aeronautics and Space Administration 1972 . 236p , Bound vol. contains NASA TN D 6880-89

Place Hold on EFFECTS OF AN IN-FLIGHT THRUST REVERSER ON THE STABILITY AND CONTROL CHARACTERISTICS OF A SINGLE-ENGINE FIGHTER AIRPLANE MODEL [NASA TN D-6886]

SUMMARY OF VGH DATA COLLECTED ON ONE TYPE OF TWIN-ENGINE JET AIRPLANE DURING AIRLINE OPERATIONS [NASA TN D-4529]

By Hunter, Paul A.. Washington, D.C. National Aeronautics and Space Administration 1968 . 32 , Bound vol. contains NASA TN D 4521-4530

Place Hold on SUMMARY OF VGH DATA COLLECTED ON ONE TYPE OF TWIN-ENGINE JET AIRPLANE DURING AIRLINE OPERATIONS [NASA TN D-4529]

SPIRIT OF ST. LOUIS

By Lindbergh, Charles Augustus. N. Y. Scribner 1953 . 562 , A Condensation Has Appeared In The Saturday Evening Post Under The Title 33 Hours To Paris

Place Hold on SPIRIT OF ST. LOUIS

Supersonic and subsonic airplane design

By Corning, Gerald. Maryland College Park 1953 . xviii, 462p

Place Hold on Supersonic and subsonic airplane design

A wind tunnel investigation of pressure flactations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane [NASA TN D-1359]

By Mckee, John W. and Thomas, A.Byrdsong. Washingto, D. C. NASA 1962 . 29p

Place Hold on A wind tunnel investigation of pressure flactations on the upper vertical tail of the X-15 when mated to the B-52 carrier airplane [NASA TN D-1359]

Flight measured wing surface presssure s and loads for the X-15 airplane ar mach numbers from 1.2 to 6.0 [NASA TN D-2601

By Pyle, Jon S.. Washington, D. C. NASA . 17p

Place Hold on Flight measured wing surface presssure s and loads for the X-15 airplane ar mach numbers from 1.2 to 6.0 [NASA TN D-2601

A flight investigation of an acceleration restrictor [NASA TN D-241]

By Assadourian, Arthur and Mallick, Donald L.. Washington, D. C. NASA 1960 . 29p

Place Hold on A flight investigation of an acceleration restrictor [NASA TN D-241]

An experimental investigation to determine the efffect of speed brake position on the longitudinal stability and trim of swept-Wing fighter airplane [NASA TN D-246]

By Taylor, Robert T.. Washingto, D. C. NASA 1960 . 46p

Place Hold on An experimental investigation to determine the efffect of speed brake position on the longitudinal stability and trim of swept-Wing fighter airplane [NASA TN D-246]

Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820

Washington NASA 1974 . various pagings

Place Hold on Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820

Discrete wall jets in quinscent air [NASA CR-2388]

By Mclean, J. D.. Washington, D. C. NASA 1974 . 42p

Place Hold on Discrete wall jets in quinscent air [NASA CR-2388]

Analog-Computer Investigation of Effects of Friction and Preload on the Dynamic Longitudinal Characteristics of a Pilot-Airplane Combination [Nasa TN D-884]

By Crane, Harold L. . Nasa Washington 1961 . 47p

Place Hold on Analog-Computer Investigation of Effects of Friction and Preload on the Dynamic Longitudinal Characteristics of a Pilot-Airplane Combination [Nasa TN D-884]

Wind tunnel tests of sevenstatic pressure probes at at transonis speeds [NASA TN D-947]

By Copone, Francis J.. Washignton, D. C. NASA 1961 . 55p

Place Hold on Wind tunnel tests of sevenstatic pressure probes at at transonis speeds [NASA TN D-947]

Local skin friction coefficients and boundary layer profiles obtained in flight from the XB-70-1 airplane at mach numbers up to 2.5 [ NASA TN D-7220 ]

By Fisher, David F.. Washington,D.C. National Aeronautics and Space Administration 1973 . 68p

Place Hold on Local skin friction coefficients and boundary layer profiles obtained in flight from the XB-70-1 airplane at mach numbers up to 2.5 [ NASA TN D-7220 ]

Upper surface blowing nacelie design study for a swept wing airplace at cruise conditions [NASA CR-2427]

By Gillette, W.B.. Washington,D.C. National Aeronautics and Space Administration 1974 . iii,123p

Place Hold on Upper surface blowing nacelie design study for a swept wing airplace at cruise conditions [NASA CR-2427]

Calculated responses of a large sweptwing airplane to continuous turbulence with flight test comparisons [ NASA TR R-69]

By Bennett, Floyd V.. Washington,D.C. National Aeronautics and Space Administration 1960 . 25p

Place Hold on Calculated responses of a large sweptwing airplane to continuous turbulence with flight test comparisons [ NASA TR R-69]

Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept wing bomber in rough air [NACA TN-4307]

By Engel, Jerome N.. Washington, D. C. National Advisory Committee for Aeronautics 1958

Place Hold on Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept wing bomber in rough air [NACA TN-4307]

Maneuverability investigation of an o3u observation airplane [Report no. 457]

By Thompson, F. L.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 14p

Place Hold on Maneuverability investigation of an o3u observation airplane [Report no. 457]

Fullscale wind tunnel investigation of the effects of a target type trust reverser on the low speed reverser on the low speed aerodynamic characreistics of asingle engine jet airplane [NASA TN D-72]

By Tolhurst, Wiliam H.. Washington, D. C. National Aeronautics and Space Administration 1959 . 42p

Place Hold on Fullscale wind tunnel investigation of the effects of a target type trust reverser on the low speed reverser on the low speed aerodynamic characreistics of asingle engine jet airplane [NASA TN D-72]

Simulation studies of stol airplane operations in metropoliton downtown and airport air traffic control environments [NASA TN D-7740]

By Sawyer, Richard H.. Washington, D. C. National Aeronautics and Space Administration 1974 . 39p

Place Hold on Simulation studies of stol airplane operations in metropoliton downtown and airport air traffic control environments [NASA TN D-7740]

Modeling of airplane performance from flight test resuls and validation with an F-104G airplane [NASA Tn D-7137]

By Marshall, Robert T.. Washington, D. C. National Aeronautics and Space Administration 1973 . 27p

Place Hold on Modeling of airplane performance from flight test resuls and validation with an F-104G airplane [NASA Tn D-7137]

Analysis of a pilot-airplane lateral instability experinced with the X-5 airplane [NASA TN D-1059]

By Taylor, Lawrence W.. Washington, D. C. National Aeronautics ad Space Administration 1961 . 29p , Bound vol. contains D-1051-1060

Place Hold on Analysis of a pilot-airplane lateral instability experinced with the X-5 airplane [NASA TN D-1059]

Landing loads and accelerations of the XB-70-1 airplane

By Wilson, Ronald J.. Washington D.C. NASA 1968 . 27p. , Bound with Accession No. 101114

Place Hold on Landing loads and accelerations of the XB-70-1 airplane

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]

Stalling and tumbling of a radio controlled parawing airplane model [NASA TN D-2291]

By LIbbey, Charles E.. Washington, D. C. National Aeronautics and Space Administration 1964 . 12p , Bound vol. contains D-2291-2300

Place Hold on Stalling and tumbling of a radio controlled parawing airplane model [NASA TN D-2291]