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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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NACA Research Memorandums
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NACA Research Memorandums
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1955
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National Advisory Committee for Aeronautics Collection
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An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98
Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9
Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
Theoretical Investigation of Laminar Heat Transfer on Yawed Infinite Cylinders in Supersonic Flow and a Comparison With Experimental Data
Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 2: blade-element performance
Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Two Aluminum-Alloy Models of 20-Inch Chord With 0.064- and 0.081-Inch-Thick Skin
A preliminary investigation of static-pressure changes associated with combustion of aluminum borohydride in a supersonic wind tunnel
Performance of Inconel 550 Turbine Blades in a Turbojet Engine and Effects of Different Forging Temperatures and Heat Treatments
Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane
Aircraft-Fuel-Tank Design for Liquid Hydrogen
Experimental investigation of methods of improving diffuser-exit total-pressure profiles for side-inlet model at Mach number 3.05
Drag Near Zero Lift of a 1/7-Scale Model of the Convair B-58 External Store as Measured in Free Flight Between Mach Numbers of 0.8 and 2.45
Investigation of impulse-type supersonic compressor with hub-tip ratio of 0.6 and turning to axial direction 2: stage performance with three different sets of stators
Experimental study of shock-positioning method of ram-jet-engine control
Static Longitudinal and Lateral Stability and Control Characteristics of an Airplane Configuration Having a Wing of Trapezoidal Plan Form With Various Tail Airfoil Sections and Tail Arrangements at a Mach Number of 6.86
A method for evaluating the loads and controllability aspects of the pitch-up problem
A study of service-imposed maneuvers of four jet fighter airplanes in relation to their handling qualities and calculated dynamic characteristics
Lift Hysteresis at Stall as an Unsteady Boundary-Layer Phenomenon
Nonlifting Wing-Body Combinations With Certain Geometric Restraints Having Minimum Wave Drag at Low Supersonic Speeds
Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds
An experimental study of applied ground loads in landing
Summary and Analysis of Horizontal-Tail Contribution to Longitudinal Stability of Swept-Wing Airplanes at Low Speeds
Rotating-stall characteristics of a rotor with high hub-tip radius ratio
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