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National Advisory Committee for Aeronautics Collection
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Wind-Tunnel Investigation at High and Low Subsonic Mach Numbers of a Thin Sweptback Wing Having an Airfoil Section Designed for High Maximum Lift
Investigation at Mach Numbers of 1.62, 1.93, and 2.41 of the Effect of Oscillation Amplitude on the Damping in Pitch of Delta-Wing-Body Combinations
Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351
Altitude performance investigation of a high-temperature afterburner
Analysis of effect of basic design variables on subsonic axial-flow-compressor performance
Experimental Investigation of Rotating Stall and Blade Vibration in the Axial-Flow Compressor of a Turbojet Engine
Combustion performance of two experimental turbojet annular combustors at conditions simulating high-altitude supersonic flight
Nitrous Oxide Supercharging of an Aircraft-Engine Cylinder
Influence of chemical composition on rupture properties at 1200 degrees F of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition
Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings
Lateral control characteristics of two structural similar flexible wings with 45 degrees sweep: a sweptback wing and a wing with M plan form
A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow
Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41
A Wind-Tunnel Investigation at High Subsonic Speeds of the Lateral Control Characteristics of Various Plain Spoiler Configurations on a 3-Percent-Thick 60 Degree Delta Wing
Effect on Transonic and Supersonic Drag of Fuselage Gloves Designed to Give a Smooth Overall Area Distribution to a Swept-Wing--Body Combination
Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts
Experimental Investigation at High Subsonic Speeds of the Rolling Stability Derivatives of a Complete Model with an Aspect-Ratio-2.52 Wing Having an Unswept 72-Percent-Chord Line and a High Horizontal tail
Rocket-powered-model investigation of the hinge-moment and normal-force characteristics of a half-diamond tip control on a 60 degree sweptback diamond wind between Mach numbers of 0.5 and 1.3
Convection of a pattern of vorticity through a shock wave
A Summary of the Low-Lift Drag and Longitudinal Trim Characteristics of Two Versions of an Interceptor-Type Airplane as Determined From Flight Tests of Rocket-Powered Models at Mach Numbers Between 0.75 and 1.78
Lateral stability and control characteristics of the Convair XF-92A delta-wing airplane as measured in flight
External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers
Supersonic-Area-Rule Design and Rocket-Propelled Flight Investigation of a Zero-Lift Straight-Wing-Body-Nacelle Configuration Between Mach Numbers 0.8 and 1.53
Full-scale wind-tunnel tests of a 35 degree swept-wing fighter airplane with a spoiler-slot-deflector lateral control system
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