Full-Scale Tunnel Measurements of the Pressures on the Elevator and Fuselage of the Curtiss XP-55 Airplane
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AIRPLANES - CURTISS P-55 (EXPERIMENTAL) WIND TUNNE↗
SEARCH · Engineering Papers
Results for “FUSELAGE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Characteristics of plain and balanced elevators on a typical pursuit fuselage at attitudes simulating normal-flight and spin conditions
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ELEVATORS - HINGE MOMENTS↗
Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions
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AIR FLOW - TAIL SURFACES↗
High-speed Wind-tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-scale Model
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GUN OPENINGS↗
Wind-tunnel Investigation of a High-critical-speed Fuselage Scoop Including the Effects of Boundary Layer
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SCOOPS↗
A Flight Investigation of Fuselage Static-pressure-vent Airspeed Installations
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INSTRUMENTS-STATIC VENTS↗
Tests of a Large Spherical Turret and a Modified Turret on a Typical Bomber Fuselage
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MACH NUMBER↗
Advanced Metallic Fuselage Cost Study
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flow forming↗
AERODYNAMIC CHARACTERISTICS IN GROUND EFFECT OF A LARGE-SCALE MODEL WITH A HIGH DISK-LOADING LIFTING FAN MOUNTED IN THE FUSELAGE
Aerodynamic characteristics in ground effect of a large scale model
AERODYNAMIC CHARACTERISTICS↗
TRANSONIC AERODYNAMIC CHARACTERISTICS OF A LATERAL CONTROL EMPLOYING ROTATABLE AIRFOILS MOUNTED VERTICALLY AT THE WING TIPS OF A 45 DEG SWEPTBACK WING, FUSELAGE, AND TAIL COMBINATION
Aerodynamic characteristics of lateral control with rotatable airfoils and sweptback wing
SWEPTBACK WING↗
EFFECT OF VERTICAL-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS
Effect of vertical tail modifications on static stability of vtol supersonic aircraft
SUPERSONIC AIRCRAFT↗
Aerodynamic Characteristics of a Spoiler-Slot-Deflector Control on a 45 deg Sweptback-Wing-Fuselage Model at High Subsonic Speeds
Lateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic speed
HINGE MOMENT↗
Prediction of first-order vibratory stresses for a propeller operating in the flow field of a wing-nacelle-fuselage combination
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Rogallo, V. L.↗
Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01
Wind tunnel determination of supersonic flow properties in vicinity swept, delta, and trapezoidal wing-body combinations
TRAPEZOIDAL WING↗
Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted lift-cruise engines for propulsion
Aerodynamic characteristics of V/STOL transport model with wing-mounted lift fans - large-scale wind tunnel investigation
LIFT FAN↗
Low-speed Aerodynamic Stability and Control Characteristics of a Cambered Fuselage, Variable-sweep Supersonic Transport Configuration
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Mc Kee, J. W.↗
Space shuttle: Effect of nacelle position, refaired fuselage, and elevator effectiveness at Mach number 0.26 for the north American Rockwell straight wing orbiter (0.00716 scale)
Low speed wind tunnel tests of effects of nacelle position, refaired fuelage, and elevator effectiveness for NAR straight wing orbiter
Tweedie, A.↗
Evaluation of a metal fuselage panel selectively reinforced with filamentary composites for space shuttle application
The use of high strength and modulus of advanced filamentary composites to reduce the structural weight of aerospace vehicles was investigated. Application of the technology to space shuttle components was the primary consideration. The mechanical properties for the boron/epoxy, graphite/epoxy, and polyimide data are presented. Structural testing of two compression panel components was conducted in a simulated space shuttle thermal environment. Results of the tests are analyzed.
Wennhold, W. F.↗