Cover Image

The influence of aerodynamic heating on the structural design of airgraft Report 207

Corporate Author:	North Atlantic Treaty Organization Advisory Group of Aeronautical Research and Development
Other Authors:	Rubes, Morris W.
Format:	Book
Language:	English
Published:	Paris North Atlantic Treaty Organization 1958
Subjects:	Αεροπλάνα, Στρατιωτικά

Similar Items

Surface warp and aerodynamic heating Report 312
Published: (1960)

The influence of aerodynamics in wind power development Report 401
Published: (1961)

Emergency stopping of airgraft which over-run airfield runways
Published: (1958)

Medical and human engineering aspects of flight in man VTOL and STOL airgraft
Published: (1959)

Some effects of internal heat sources on the design of flight structures Report 208
Published: (1958)

Aerodynamic problems of motor cars Report 307
Published: (1960)

Theory of structural design Report 214
Published: (1958)

The use of wind tunnels in industrial aerodynamic research Report 309
Published: (1960)

Boundary layer separation in the presence of heat transfer Report 280
Published: (1960)

Turbulent boundary layers with heat transfer in compressible flow Report 281
Published: (1960)

Development of the spark - heated, hypervelocity, blowdown tunnel - hotshot Report 233
Published: (1958)

An experimental technique to measure heat transfer fluxes at high speeds:Turbulent heat transfer data on a blunt body at M=3.98 Report 284
Published: (1960)

Missile structures and materials Report 218
Published: (1958)

Real - gas laminar boundary layer skin friction and heat transfer Report 282
Published: (1960)

Cooling of structures in high speed flight Report 210
Published: (1958)

Cyclic temperature effects on materials and structures Report 410
Published: (1962)

Consideration of human factors in helicopter design Report 238
Published: (1959)

Effects of heat transfer on laminar boundary layer development under pressure gradients in compressible flow Report 279
Published: (1960)

On models for the probability of fatigue failure of a structure Report 245
Published: (1959)

Design and operation of the X-15 hypersonic research airplane Report 288
Published: (1960)

The place of servo-mechanisms in the design of aircraft with good flight characteristics Report 360
Published: (1961)

A design philosophy for repeated thermal loading
Published: (1958)

An initial assessment of graphite as a structural material in conditions of high thermal flux
Published: (1960)

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle
Published: (1959)

Vertical instruments Report 404
Published: (1962)

Corner interference effects Report 299
Published: (1959)

The case for adaptive controls Report 406
Published: (1962)

Advanced cockpit instrumentation Report 235
Published: (1959)

On the stability of coutte flow Report 265
Published: (1960)

The flight testing of aircraft weapon systems Report 287
Published: (1960)

Remarks on the status of project mercury Report 290
Published: (1960)

Support interference at supersonic speeds Report 300
Published: (1959)

The X-15 research program Report 289
Published: (1960)

Methods of flight testing in the Soviet Union Report 234
Published: (1959)

Industrial applications of wind tunnel investigations Report 314
Published: (1960)

Flight testing of the Fiat G91 Report 315
Published: (1961)

Aliasing errors in sampled data systems Report 316
Published: (1961)

On the nonlinear approach to the aeroelastic stability theory Report 246
Published: (1959)

Stability of the compressible laminar boundary layer Report 268
Published: (1960)

Boundary layers in three dimensions Report 273
Published: (1960)

Cannot write session to /tmp/vufind_sessions/sess_r74fs01j7onqfgcgihbvul4ki6