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Now showing items 1331-1350 of 3498

GeoSAR Feasibility Study: Summary of the Group Design Project. MSc in Astronautics and Space Engineering 2012/13

Hobbs, Stephen (Cranfield University, )
GeoSAR: Summary of the Group Design Project MSc in Astronautics and Space Engineering 2005/06 Cranfield University

Hobbs, Stephen
Glide-path stability of an aircraft under speed constraint

W. J. G. Pinsker (1971)

The motion of an aircraft operating under perfect speed constraint (e.g. by an appropriate autothrottle) is examined theoretically and it is shown that, if engine thrust acts through the aircraft centre of gravity, the ...
Gradient properties of a model of stationary random turbulence

J. G. Jones (1968)
GRAMPA--an automatic technique for exciting the principal modes of vibration of complex structures

F.J. Hawkins (1965)

This Report describes a new technique for finding automatically, when using multipoint excitation, the force distribution required to produce in-phase responses at the excitation points on a structure. It is shown how this ...
Graphical method of calculating performance of airscrew

Lock, C. N. H. (H. M. Stationery Office, 1934-10)

A rapid method is described of making calculations of airscrew performance by means of charts. The first application is to ordinary strip theory calculations on the basis of the formulae of Ref. 5. Six charts are required ...
A graphical method of predicting the off design performance of a compressor stage

J. F. Louis; J. H. Horlock (1957)
Graphical solution of multhopp's equations for the lift-distribution of wings

F. Vandrey (1952)
Graphical treatment of binary mass-balancing problems

R. A. Frazer (1942)

A graphical method, based on 'classical' flutter theory, is described which provides a simple test of the effectiveness of mass-balancing in the prevention of flutter at various heights. Illustrative applications are made ...
Graphite as a structural material in conditions of high thermal flux: a survey of existing knowledge and an assessment of current research and development

Kennedy, A. J. (College of Aeronautics, )
Grinding cycle control project 1967

Boshier, G. C. (College of Aeronautics, )
Grinding theory

Hillier, M. J. (College of Aeronautics, )
Ground effect on a 55 degrees swept M-wing of aspect ratio 5.0

L. A. Wyatt (1961)
Ground level disturbance from large aircraft flying at supersonic speeds

Lilley, G. M.; Spillman, J. J. (College of Aeronautics, )
The growth of compressible turbulent boundary layers on isothermal and adiabatic walls

D. A. Spence (1959)

A recent study of velocity profiles in the turbulent boundary layer on a flat plate at high Mach numbers has suggested the formula for relating the form parameter H to its incompressible value Hi. This formula is used in ...
Growth of the turbulent wake close behind an aerofoil at incidence

D. A. Spence (1953)
Guided weapons aerodynamic study force and moment measurements on some monoplane and cruciform slender wing-body combinations at M 4. 0

P. L. Roe (1968)
Gun tunnel force measurements on some thin delta wings suitable for hypersonic cruising flight

T. Opatowski (1971)
Gun tunnel measurements of lift, drag and pitching moment on a 20 degrees cone, a flat delta and a caret delta wing at a mach number of 8.3

T. Opatowski (1966)
Gust alleviation factor. Parts I, II and III

J. K. Zbrozek (1953)

Part I. The report presents the theoretical calculations of gust alleviation factor made for rigid aircraft and with one degree of freedom only (i.e., vertical motion). It is shown that for average gust lengths and for ...

Now showing items 1331-1350 of 3498

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