Tests on a model of the D.F.W. airplane T-29 of the "Deutsche Flugzeug derke" (German airplane works) [PDF]
Experiments similar to those carried out with the A.E.G (Allgemeine Elektrizitats-Gesellschaft) were made in the small wind tunnel of the Gottingen laboratory on a model of the D.F.W. airplane T-29.
Molthan, Wilhelm
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Forebody and vertical stabilizer effects on directional stability of a reusable LOX/RP (061) booster AR 12161-2 [PDF]
Results are presented of a wind tunnel test on the directional stability of space shuttle booster configurations. The test was conducted at the 14-inch trisonic tunnel starting 6 December 1971 and continued through 11 December 1971 for a total of 66 ...
Ainsworth, R. W. +2 more
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Results of transonic wind tunnel tests on an 0.015-scale space shuttle mated vehicle model (67-ots) in the LaRC 8 foot TPT (IA41) [PDF]
Wind tunnel tests were conducted to obtain aerodynamic force data for Mach numbers from 0.60 to 1.20. Data were obtained for an alpha range of -10 deg to +10 deg (beta = 0 deg beta = 5 deg) and beta range of -10 deg to +10 deg (alpha = 0 deg ...
Burrows, R. R., Hardin, R.
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Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems [PDF]
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass properties and whose attitudes are controlled by both aerodynamic surfaces and reaction control system thrusters was developed.
Powell, R. W. +2 more
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Pilot dynamic response to sudden flight control system failures and implications for design [PDF]
Pilot dynamic response to sudden flight control system ...
Johnson, W. A., Weir, D. H.
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Extraction from flight data of lateral aerodynamic coefficients for F-8 aircraft with supercritical wing [PDF]
A parameter-extraction algorithm was used to determine the lateral aerodynamic derivatives from flight data for the F-8 aircraft with supercritical wing.
Suit, W. T., Williams, J. L.
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Harmonic adaptive fault-tolerant control for incipient and multiple faults of high mobility fighter. [PDF]
Sci RepHu K, Wang Z, Wang J.
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Limited evaluation of an F-14A airplane utilizing an aileron-rudder interconnect control system in the landing configuration [PDF]
A flight test was conducted for preliminary evaluation of an aileron-rudder interconnect (ARI) control system for the F-14A airplane in the landing configuration.
Enevoldson, E. K., Kelley, W. W.
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