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    The I.Ae.S. Annual Meeting

    A Summary of the Papers Read to the Members of the Institute of the Aeronautical Sciences
    Klemin, Alexander | Emerald Group Publishing | 1938

    SINCE its inception, but a few years ago, the Institute of the Aeronautical Sciences has grown remarkably in the size and distinction of

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    Sound Publicity

    Emerald Group Publishing | 1948
    members of the Industry, belong to the Institute and therefore see its journal regularly. Nor need we, perhaps, we feel, express any deep ...

    Getting Down to Laminar Flow

    Emerald Group Publishing | 1948

    AS some of our readers will be aware, PROFESSOR GOLDSTEIN'S Wright-Brothers lecture appears in the April issue of the Journal of

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    Food for Thought

    Emerald Group Publishing | 1951
    title of one which seemed likely to be of interest to our readers and we therefore wrote to the SOCIETY OF AUTOMOTIVE ENGINEERS for a copy. On ...

    Technical Education

    Emerald Group Publishing | 1956

    MANY months of discussion about ways of making good the scarcity of technologists in all the engineering industries, and in the aircraft

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    Investigation of optimal zoom climb techniques

    Kelley, H.J. | Engineering Index Backfile | 1959
    Problem of zoom climb maneuvering of turbojet aircraft is studied using Mayer formulation of calculus of variations; Euler-Lagrange ...

    Dynamics and thermodynamics of re-entry

    Loh, W.H.T. | Engineering Index Backfile | 1960
    Summary of approximate analytical solutions on velocity, altitude, range, deceleration, maximum deceleration, time rate and maximum time ...

    Epicycle method for reduction of flight-test data using digital computer

    Danis, R.P. | Engineering Index Backfile | 1960
    angular rates and linear accelerations; solution of equations of motion for angular velocity can be represented as sum of two rotating vectors ...
    Keywords: Rockets and missiles

    A Method of Reducing Aeroelastic Effects of Highly Swept Wings

    Hopkins, Edward J. / Jillie, Don W. / Hicks, Raymond M. | NTRS | 1960
    wing with 60deg of sweepback and designed for a Mach number of 2.0. The wing shown was found theoretically to have considerable loss in maximum ...
    Publisher: NASA National Aeronautics and Space Administration

    Application of power spectral methods in airplane and missile design

    Thorson, K.R. / Bohne, Q.R. | Engineering Index Backfile | 1960
    Applications of methods in determination of dynamic loadings and response for both aircraft and missiles subject to continuous turbulence ...

    Theory of supersonic-propeller aerodynamics

    Ordway, D.E. / Hale, R.W. | Engineering Index Backfile | 1960
    linearized theory; exact potential for helical acoustic source is developed and approximated; distribution of sources and relationship of blade ...

    Optimization of flight-control, airframe system

    Ashkenas, I.L. / McRuer, D.T. | Engineering Index Backfile | 1960
    Overall approach considering both airframe and flight controller to be alterable system elements, making use of servo techniques; attention ...

    On estimation of structural damping from aircraft resonance tests

    Milne, R.D. | Engineering Index Backfile | 1960
    Within framework of linearized "complex" damping, method is proposed for estimating, from ground resonance tests on prototype aircraft ...

    Terminal guidance for rendezvous in space

    Wiltshire, R.S. / Clohessy, W.H. | Engineering Index Backfile | 1960
    with satellite inspection; terminal guidance system would be composed of radar, digital computer and propulsion system. (See also Astronautical ...

    Effect of controlled three-dimensional roughness on boundary-layer transition at supersonic speeds

    Van Driest, E.R. / McCauley, W.D. | Engineering Index Backfile | 1960
    recovery measurements, and surface flow pattern indicators; pertinence to design of high altitude glide vehicles and hypersonic re-entry bodies. ...

    On thrust hypothesis for jet flap including jet-mixing effects

    Yen, K.T. | Engineering Index Backfile | 1960
    Linearized problem of jet-flap system is found to be linear combination of lift problem and thrust problem; lift problem gives all lift ...

    Trends in VTOL aircraft propulsion system requirements

    Nichols, J.B. | Engineering Index Backfile | 1960
    at Hiller Aircraft Corp; development of "integrated" aircraft, jet flap, and Ring Wing, or " Coleopter"; Lift Propulsor type, or wingless ...

    Wings with minimum drag due to lift in supersonic flow

    Ginzel, I. / Multhopp, H. | Engineering Index Backfile | 1960
    and actual shape of lifting surface. ...

    Role of entropy in aerospace sciences

    Ackeret, J. | Engineering Index Backfile | 1961
    Review of state of aerothermodynamics in light of concept of entropy; enthalpy and free enthalpy; propulsion in void; entropy in gas flow ...

    Velocity and range considerations for attainment of given intercept angles

    Tempelman, W.H. | Engineering Index Backfile | 1961
    circular orbit with final altitudes of 450,000 ft and 1028 n mi in graphical form. ...