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 Collection: National Advisory Committee for Aeronautics Collection
Spin tests of two models of a low-wing monoplane to investigate scale effect in the model test range
No Description digital.library.unt.edu/ark:/67531/metadc279675/
Westland "Wessex" commercial airplane (British) : a high-wing semicantilever monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279638/
Breguet 390 T commercial airplane (French) : a ten-seat all-steel sesquiplane
No Description digital.library.unt.edu/ark:/67531/metadc279625/
The S.A.B.C.A. "S.XI" commercial airplane (Belgian) : a high-wing semicantilever monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279656/
Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system
No Description digital.library.unt.edu/ark:/67531/metadc279610/
Ditching tests with 1/10-size model of the Army A-20A airplane I : calm-water tests in NACA tank no.2
No Description digital.library.unt.edu/ark:/67531/metadc279645/
The Armstrong Whitworth A.W. XVI military Airplane (British) : a single-seat biplane
No Description digital.library.unt.edu/ark:/67531/metadc279647/
The "I.A.R." pursuit airplane (Roumanian) : a one-place cantilever low-wing monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279651/
The use of geared spring tabs for elevator control
No Description digital.library.unt.edu/ark:/67531/metadc279612/
The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow
No Description digital.library.unt.edu/ark:/67531/metadc279634/
Lift theory of supporting surfaces : second article
No Description digital.library.unt.edu/ark:/67531/metadc279655/
Nieuport-Delage 640 (French) : commercial high-wing monoplane
The Nieuport Delage 640 is a single engine commercial high-wing monoplane of all wood construction, including the fuselage and tail. It's landing gear is hinged in two parts. digital.library.unt.edu/ark:/67531/metadc279648/
Liore-Olivier airplane : type 12 night-bomber or type 20 commercial
No Description digital.library.unt.edu/ark:/67531/metadc279601/
An investigation of a thermal ice-prevention system for a C-46 cargo airplane IV : results of flight tests in dry-air and natural-icing conditions
No Description digital.library.unt.edu/ark:/67531/metadc279606/
Flight measurements of the effect of various amounts of aileron droop on the low-speed lateral-control characteristics of an observation airplane
No Description digital.library.unt.edu/ark:/67531/metadc279604/
The D.H. 85 "Leopard Moth" airplane (British) : a three-seat cabin high-wing monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279636/
Performance of an exhaust-gas "blowdown" turbine on a nine-cylinder radial engine
No Description digital.library.unt.edu/ark:/67531/metadc279622/
The A.N.E.C. IV "Missel Thrush" light airplane
A product of the Air Navigation Engineering Co., the Missel Thrush is a light airplane suitable for private ownership. It is a two seat tractor fuselage biplane with single I interplane struts designed by J. Bewsher. digital.library.unt.edu/ark:/67531/metadc279637/
Determination of general relations for the behavior of turbulent boundary layers
No Description digital.library.unt.edu/ark:/67531/metadc279609/
The development and application of high-critical-speed nose inlets
No Description digital.library.unt.edu/ark:/67531/metadc279653/
The Stieger ST. 4 light airplane (British) : a twin-engine four-seat low-wing cabin monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279679/
D.H. 86 "Express Air Liner" (British) : a four-engine biplane
No Description digital.library.unt.edu/ark:/67531/metadc279667/
An experimental study of five annular air inlet configurations at subsonic and transonic speeds
No Description digital.library.unt.edu/ark:/67531/metadc279680/
The De Havilland 61 "Canberra" (British) : a 6-8 passenger airplane
Made for an Australian buyer, the Canberra is capable of carrying a payload of 1900 lbs. with a top speed of 126 M.P.H. At 105-110 M.P.H. it has a range of about 475 miles. It has a single Jupiter VI engine. digital.library.unt.edu/ark:/67531/metadc279646/
Les Mureaux "130.A2" observation airplane (French) : a high-wing two-seat monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279661/
The Francois Villiers marine pursuit airplane
A traditional biplane design allows this craft to function with the speed and maneuverability necessary to perform as a pursuit aircraft while also being able to land on water. It featured retractable landing gear for water landings. It was powered with a 450 HP. Lorraine-Dietrich engine. digital.library.unt.edu/ark:/67531/metadc279671/
Thermodynamic design of double-panel, air-heated windshields for ice prevention
No Description digital.library.unt.edu/ark:/67531/metadc279628/
Wind-tunnel investigation to determine the horizontal- and vertical-tail contributions to the static lateral stability characteristics of a complete-model swept-wing configuration at high subsonic speeds
No Description digital.library.unt.edu/ark:/67531/metadc279650/
An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling
No Description digital.library.unt.edu/ark:/67531/metadc279654/
Flight studies of the horizontal-tail loads experienced by a fighter airplane in abrupt maneuvers
No Description digital.library.unt.edu/ark:/67531/metadc279611/
The Bleriot 110 airplane (French) : a long-distance high-wing monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279624/
The Dewoitine D 33 commercial airplane (French) : a low-wing cantilever monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279652/
The Westland IV commercial monoplane (British)three "Cirrus III" engine
No Description digital.library.unt.edu/ark:/67531/metadc279633/
The Short "Calcutta" : first British all-metal commercial seaplane
The Calcutta is a large seaplane, with seating for 16 and a payload of 3,400 pounds. digital.library.unt.edu/ark:/67531/metadc279641/
NACA Mach number indicator for use in high-speed tunnels
No Description digital.library.unt.edu/ark:/67531/metadc279639/
Bleriot-Spad 91 Airplane (French) : pursuit single-seater, type "Jockey"
This aircraft has announced a speed of 270 km per hour at 4000 m. It is of all metal construction. digital.library.unt.edu/ark:/67531/metadc279665/
The boundary layer as a means of controlling the flow of liquids and gases
According to one of the main propositions of the boundary layer theory the scarcely noticeable boundary layer may, under certain conditions, have a decisive influence on the form of the external flow by causing it to separate from the wing surface. These phenomena are known to be caused by a kind of stagnation of the boundary layer at the point of separation. The present report deals with similar phenomena. It is important to note that usually the cause (external interference) directly affects only the layer close to the wall, while its indirect effect extends to a large portion of the external flow. digital.library.unt.edu/ark:/67531/metadc279635/
Rocket-model investigation to determine the hinge-moment and normal-force properties of a full-span, constant-chord, partially balanced trailing-edge control on a 60 degree clipped delta wing between Mach numbers of 0.50 and 1.26
No Description digital.library.unt.edu/ark:/67531/metadc279664/
The Comper "Streak" single seat airplane (British) : a low-wing cantilever monoplane
No Description digital.library.unt.edu/ark:/67531/metadc279605/
An investigation of a thermal ice-prevention system for a C-46 cargo airplane VI : dry-air performance of thermal system at several twin- and single-engine operating conditions at various altitudes
No Description digital.library.unt.edu/ark:/67531/metadc279617/
An investigation of a thermal ice-prevention system for a C-46 cargo airplane V : effect of thermal system on airplane cruise performance
No Description digital.library.unt.edu/ark:/67531/metadc279663/
A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel
No Description digital.library.unt.edu/ark:/67531/metadc279629/
On the flow of a compressible fluid by the hodography method I : unification and extension of present-day results
No Description digital.library.unt.edu/ark:/67531/metadc279666/
A polar-coordinate survey method for determining jet-engine combustion-chamber performance
No Description digital.library.unt.edu/ark:/67531/metadc57811/
Study of screeching combustion in a 6-inch simulated afterburner
No Description digital.library.unt.edu/ark:/67531/metadc57817/
Wind-tunnel investigation of horizontal tails IV : unswept plan form of aspect ratio 2 and a two-dimensional model
No Description digital.library.unt.edu/ark:/67531/metadc57810/
The effect of air jets simulating chines or multiple steps on the hydrodynamic characteristics of a streamline fuselage
No Description digital.library.unt.edu/ark:/67531/metadc57818/
Free-flight investigation of the rolling effectiveness at high subsonic, transonic, and supersonic speeds of leading-edge and trailing-edge ailerons in conjunction with tapered and untapered plan forms
No Description digital.library.unt.edu/ark:/67531/metadc57814/
Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness
No Description digital.library.unt.edu/ark:/67531/metadc57819/
Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings
No Description digital.library.unt.edu/ark:/67531/metadc57816/