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Technical Report Archive and Image Library
24
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Technical Report Archive and Image Library
24
National Advisory Committee for Aeronautics Collection
17
TRAIL Microcard Collection
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NACA Research Memorandums
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NACA Research Memorandums
16
Hanford Works Reports
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United States
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1956
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1956
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14th
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14th
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Technical Report Archive and Image Library
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1956
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PRPR Control Requirements. Part I.
Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3
A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through a Rate Type of Automatic Control System
A Semiempirical Procedure for Estimating Wing Buffet Loads in the Transonic Region
Transonic Wind-Tunnel Investigation of Static Longitudinal Force and Moment Characteristics of Two Wing-Body Combinations With Clipped-Tip and Full Delta Wings of Aspect Ratio 1.73
Use of a diffuser Mach number as a supersonic-inlet control parameter
Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395
Electronics Counting Rooms for Nuclear Research
Experimental investigation of interference effects of lateral-support struts on afterbody pressures at Mach 1.9
Feasibility of In Vivo Plutonium Measurements
Final Report: Corrosion of Types 304-L and 347 Stainless Steel by Oxalic Acid
Gas-to-blade heat-transfer coefficients and turbine heat-rejection rates for a range of one-spool cooled-turbine engine designs
Heat-Requirements for Ice Protection of a Cyclically Gas-Heated, 36 Degree Swept Airfoil with Partial-Span Leading-Edge Slat
Investigation of Afterburner Combustion Screech and Methods of Its Control at High Combustor Pressure Levels
Use of effective momentum thickness in describing turbine rotor-blade losses
Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow
Neutron Irradiation of Sapphire (Al 2 O 3 )
Studies on the Hydraulic Characteristics of Purex Off-Gas Jets
Aerodynamic heating of aircraft components
Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9
A flight evaluation of a wing-shroud-blowing boundary-layer control system applied to the flaps of an F9F-4 airplane
Gas Pressurization of Homogeneous Reactor Test
Simulated flight investigation of scaled-speed elastic swept-wing bomber and fighter models coupled wing tip to wing tip
Simulated Flight Investigation of Scaled-Speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip
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