Synonyms were used for: Aircraft Design
Search without synonyms: title: Aircraft Aerodynamic Design

21–40 of 335 hits
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    Two-Stage Axial Compressor Rig Designed To Develop and Validate Advanced Aerodynamic Technologies

    Larosiliere, Louis M. | NTRS | 2003
    aerodynamic design capability is required not only to maximize the specific thrust of next-generation engines without sacrificing fuel consumption ...
    Keywords: Aircraft Propulsion And Power

    Transonic transport wings - Oblique or swept

    Jones, R. T. / Nisbet, J. W. | NTRS | 1974
    Oblique-wing twin- and single-fuselage transonic transport models were wind tunnel tested and showed superior aerodynamic efficiency to ...
    Keywords: Aircraft Design, Testing And Performance

    Transonic Investigation of Aerodynamic Characteristics of a Swept-Wing Fighter-Airplane Model with Leading-Edge Droop in Combination with Outboard Chord-Extensions and Notches

    Whitcomb, Charles F. / Norton, Harry T., Jr. | NTRS | 1961
    An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing ...
    Keywords: Aircraft Design, Testing And Performance

    Transonic flutter and gust-response tests and analyses of a wind-tunnel model of a torsion-free-wing fighter airplane

    Ruhlin, C. L. / Murphy, A. C. | NTRS | 1981
    of a 1/5.5-size complete-airplane version of a torsion-free-wing (TFW) fighter aircraft. The critical flutter mode for the TFW-free ...

    Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC

    Brett Hiller / Richard Campbell / Michelle Banchy | NTRS
    A knowledge-based aerodynamic design method, CDISC, has been extended to enable the computational design of transonic cruise slotted wings ...
    Keywords: Aerodynamic Design

    Transonic aeroelastic analysis of the B-1 wing

    Guruswamy, G. P. / Goorjian, P. M. / Ide, H. et al. | NTRS | 1986
    numbers. The aerodynamic and aeroelastic computations are made by using the transonic unsteady code ATRAN3S. Steady aerodynamic computations ...
    Keywords: Aircraft Design, Testing And Performance

    Transonic aerodynamics; Transonic Perspective Symposium, Moffett Field, CA, February 18-20, 1981, Technical Papers

    Nixon, D. | NTRS | 1982
    design for cruise performance efficiency of commercial transport aircraft, with emphasis on transonic wing design, the practical aerodynamic ...

    Transonic Aerodynamic and Trim Characteristics of a Multi-engine Delta-wing Airplane Model

    Foss, W. E., Jr. / Swihart, J. M. | NTRS | 1956
    Wind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise increment and maximum lift-drag ratio ...
    Keywords: AIRCRAFT DESIGN

    Transition to space - A history of 'space plane' concepts at Langley Aeronautical Laboratory 1952-1957

    Hansen, James R. | NTRS | 1987
    The supersonic speeds of X-series aircraft and wind tunnel data in the early 1950s demonstrated that hypersonic flight was an achievable ...

    Training aircraft design considerations based on the successive organization of perception in manual control

    Heffley, R. K. / Clement, W. F. / Craig, S. J. | NTRS | 1982
    determination of design point approach speeds as well as other important aerodynamic features for training aircraft is also considered. Two keys are ...

    Total aircraft flight-control system - Balanced open- and closed-loop control with dynamic trim maps

    Smith, G. A. / Meyer, G. | NTRS | 1979
    complete nonlinear propulsive and aerodynamic data for the aircraft to construct dynamic trim maps that represent an inversion of the aircraft ...
    Keywords: Aircraft Stability And Control

    The Road to Mach 10: A History of the X-43A Hypersonic Flight Test Program at NASA Dryden...Toward the Future

    Peebles, Curtis | NTRS | 2007
    tests, proposals, and canceled projects, a scramjet-powered vehicle had flown. The performance of the engine qualified the scramjet design tools ...
    Keywords: Aircraft Design, Testing And Performance

    The NASA Aircraft Energy Efficiency program

    Klineberg, J. M. | NTRS | 1979
    propulsive, aerodynamic and structural efficiency for future transport aircraft. Attention is given to engine component improvement, an energy ...
    Keywords: Aircraft Design, Testing And Performance

    The influence of wing, fuselage and tail design on rotational flow aerodynamics data obtained beyond maximum lift with general aviation configurations

    Bihrle, W., Jr. / Bowman, J. S., Jr. | NTRS | 1980
    to support this effort. Located in the Langley spin tunnel, this system makes it possible to identify an airplane's aerodynamic ...
    Keywords: Aircraft Stability And Control

    The Flying V A new Aircraft Configuration for Commercial Passenger Transport

    Benad, J. | DataCite | 2015
    configuration proposal was made with this idea. This configuration was then compared with a reference aircraft. The idea is to arrange two cylindrical ...
    Keywords: unconventional aircraft configuration

    The feasibility of large sonic boom reductions

    Busemann, A. | NTRS | 1968
    Linearized supersonic aerodynamic design theory for large sonic boom reduction ...
    Keywords: Aircraft

    The Effects of Aerodynamic Heating on Ice Formations on Airplane Propellers

    Rodert, Lewis A. | NTRS | 1940
    An investigation has been made of the effect of aerodynamic heating on propeller-blade temperatures. The blade temperature rise resulting ...
    Keywords: Aircraft Design, Testing And Performance

    The Effect of Lower Surface Spoilers on the Transonic Trim Change of a Wind-Tunnel Model of a Fighter Airplane Having a Modified Delta Wing

    Robinson, Robert C. | NTRS | 1959
    In an attempt to find an aerodynamic means of counteracting the transonic trim change of a fighter airplane, lower surface spoilers were ...
    Keywords: Aircraft Design, Testing And Performance

    The effect of canard leading edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristic of a close-coupled canard-wing configuration

    Gloss, B. B. | NTRS | 1974
    A generalized wind-tunnel model, with canard and wing planforms typical of highly maneuverable aircraft, was tested in the Langley high ...
    Keywords: Aircraft Design, Testing And Performance

    The Effect of an Operating Propeller on the Aerodynamic Characteristics of a 1/10-Scale Model of the Lockheed XFV-1 Airplane at High Subsonic Speeds (TED No. NACA DE-377)

    Sutton, Fred B. / Buell, Donald A. | NTRS | 1952
    aerodynamic characteristics of a l/l9-scale model of the Lockheed XFV-1 airplane, Several full-scale power conditions were simulated at Mach numbers ...
    Keywords: Aircraft Design, Testing And Performance