The effect on profile drag of randomly distributed, low - intensity roughness Report 257

Corporate Author:	North Atlantic Treaty Organization Advisory Group of Aeronautical Research and Development
Other Authors:	Coleman, W. S.
Format:	Book
Language:	English
Published:	Paris North Atlantic Treaty Organisation 1960
Subjects:	Αεροπλάνα, Στρατιωτικά

Similar Items

Effect of roughness on transition in supersonic flow Report 255
Published: (1960)

Review of the effect of distributed surface [report 254] : roughness on boundary - layer transition
Published: (1960)

Recent developments in the field of low drag boundary layer suction research Report 262
Published: (1960)

Effects of unit Reynolds number, nose bluntness, and roughness on boundary layer transition Report 256
Published: (1960)

Corner interference effects Report 299
Published: (1959)

Non - aeronautical applications of low-speed wind tunnel techniques Report 313
Published: (1960)

Calculation of the turbulent boundary layer with continuously distributed suction Report 259
Published: (1960)

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

Effects of servo-mechanism characteristics on aircraft stability and control Report 361
Published: (1961)

Ground effect machines
Published: (1962)

Tunnel-wall effects associated with VTOL-STOL model testing Report 303
Published: (1959)

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

Large angle of attack model - sting interference effects at transonic speeds Report 301
Published: (1959)

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

Some effects of wind tunnel interference observed in tests on two-dimensional aerofoils at high subsonic and transonic speeds Report 296
Published: (1959)

An investigation of interference effects on similar models of different size in various transonic tunnels in the United Kingdom Report 297
Published: (1959)

The effectiveness of the transonic wind tunnel as a device for minimizing tunnel - boundary interference for model tests at transonic speeds Report 294
Published: (1959)

Bio-assay techniques for human centrifuges and physiological effects of acceleration
Published: (1961)

Vertical instruments Report 404
Published: (1962)

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

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

Theory of structural design Report 214
Published: (1958)

Missile structures and materials Report 218
Published: (1958)

Advanced cockpit instrumentation Report 235
Published: (1959)

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

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

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

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

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

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

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

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

Characteristics of separated cylindrical boundary layers Report 261
Published: (1960)

Experimental research on the mechanism of transition Report 263
Published: (1960)

Three - dimensional laminar instability Report 266
Published: (1960)

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

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

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

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

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

Cannot write session to /tmp/vufind_sessions/sess_edodbuqkl0jjb5frvkhojm1795