Search

17 items

full text unavailable
Spin and Recovery Tests of a 1/28-Scale Model of the YF-93A Airplane
Author(s): Rose, Eugene S., Jr., Parker, Dan M.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-206
full text unavailable
Rigid Tow Bar for C-82 Type Aircraft
Author(s): Jones, Arthur G.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-167
full text unavailable
A Development of the Longitudinal Dynamic Equations of Motion of an Aircraft at the Absolute Ceiling
Author(s): Robinson, Alfred C., Doody, Bernard J.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1955-05
Report number: WADC TR 55-210
full text unavailable
The Air Force Program For Improved Flight Instrumentation
Author(s): Wright, Lawrence C.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-11
Report number: WADC TR 56-582
full text unavailable
Simulation Study Of Control Of An Aircraft At Or Near The Absolute Ceiling
Author(s): Robinson, Alfred C., Early, James W., Doody, Bernard J.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-03
Report number: WADC TR 56-39
full text unavailable
The Effects Of Engine Angular Momentum On An Airplane's Longitudinal And Lateral-Directional Dynamic Stability
Author(s): Paiewonsky, Bernard H.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-225
full text unavailable
A Method for Estimating Damping Derivatives of VTOL Aircraft in Transition and Hovering Flight
Author(s): Paiewonsky, Bernard H.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-410
full text unavailable
Investigation of a Technique for Improving Aircraft Response Using a Complementary Optimum-Response Model
Author(s): Rath, Raymond R.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-475
application/pdf thumbnail
full text available
An Analytical Method for the Classification of Flow Areas of Supersonic Wings
Author(s): Mallett, Frank M.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1960-08
Report number: WADC TR 58-669
application/pdf thumbnail
full text available
Air Research Development Command Plans and Programs
Author(s): Gregory, P. C.
Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1961-03
Report number: WADC TR 59-49 p. 8-10