Results 91 to 100 of about 899,057 (211)
Comparison of closed loop model with flight test results [PDF]
An analytic technique capable of predicting the landing characteristics of proposed aircraft configurations in the early stages of design was developed.
George, F. L.
core +1 more source
Engine exhaust characteristics evaluation in support of aircraft acoustic testing [PDF]
NASA Dryden Flight Research Facility and NASA Langley Research Center completed a joint acoustic flight test program. Test objectives were (1) to quantify and evaluate subsonic climb-to-cruise noise and (2) to obtain a quality noise database for use in ...
Ennix, Kimberly A.
core +1 more source
A Flight Test of the Strapdown Airborne Gravimeter SGA-WZ in Greenland. [PDF]
Zhao L +5 more
europepmc +1 more source
Comparison of real flight test with simulator flight test
In dieser Arbeit geht es um den Vergleich von realen Flugversuchen mit Simulatorflugversuchen. Die realen Tests werden mit einer Reims/Cessna 172P Skyhawk auf dem Flughafen Linz durchgeführt. Die Simulatorflugtests werden mit dem Microsoft Flight Simulator (MSFS) und X-Plane 12 mit der Cessna 172SP durchgeführt, die in beiden Simulatoren enthalten ist.
openaire +1 more source
SSME propulsion performance reconstruction techniques [PDF]
In view of the complex flight operation of the Space Shuttle propulsion system together with an expected launch rate increase, the flight performance reconstruction process needs to be performed by automated computer programs.
Temple, Enoch C.
core +1 more source
Aerodynamics for the ADEPT SR-1 Flight Experiment [PDF]
Adaptable, Deployable, Entry, and Placement Technology (ADEPT) is a combination of a heatshield and an aerodynamic decelerator for atmospheric entry applications.
Dutta, Soumyo +4 more
core +1 more source
Expanded study of feasibility of measuring in-flight 747/JT9D loads, performance, clearance, and thermal data [PDF]
The JT9D jet engine exhibits a TSFC loss of about 1 percent in the initial 50 flight cycles of a new engine. These early losses are caused by seal-wear induced opening of running clearances in the engine gas path.
Martin, R. L., Sallee, G. P.
core +1 more source
Reconstruction of the Advanced Supersonic Parachute Inflation Research Experiment Sounding Rocket Flight Test [PDF]
The Advanced Supersonic Parachute Inflation Research and Experiments project is a flight test program for development of supersonic parachutes for potential future use at Mars. The flight tests are designed to reduce risk for the Mars 2020 mission.
Karlgaard, Christopher D. +2 more
core +1 more source
Rotor systems research aircraft airplane configuration flight-test results [PDF]
The rotor systems research aircraft (RSRA) has undergone ground and flight tests, primarily as a compound aircraft. The purpose was to train pilots and to check out and develop the design flight envelope.
Erickson, R. E., Painter, W. D.
core +1 more source

