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Primary view of Wind-Tunnel Tests of a Swept-Blade Propeller and Related Straight Blades Having Thickness Ratios of 5 and 6 Percent
Gray, W. H.
November 10, 1948
Primary view of Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane
Kelly, Mark W. & Tucker, Jeffrey H.
October 26, 1956
Primary view of Wind-Tunnel Tests of the 1/25-Scale Powered Model of the Martin JRM-1 Airplane. 4 - Tests with Ground Board and with Modified Wing and Hull - TED No. NACA 232, Part 4, Tests with Ground Board and with Modified Wing and Hull, TED No. NACA 232
Lockwood, Vernard E. & Smith, Bernard J.
September 4, 1947
Primary view of Wind-Tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-Wing Airplane With Blowing Flaps and Leading-Edge Slats
James, Harry A. & Maki, Ralph L.
July 5, 1957
Primary view of Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats
James, Harry A. & Maki, Ralph L.
July 5, 1957
Primary view of Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with slotted flaps, area-suction flaps, and wing leading-edge devices
Maki, Ralph L. & James, Harry A.
April 30, 1957
Primary view of Wind-Tunnel Tests to Determine Aileron Characteristics of the McDonnell XFD-1 Airplane, TED No. NACA 23102
Yates, Campbell C. & Schneiter, Leslie E.
September 26, 1946
Primary view of Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
Jorgensen, Leland H. & Katzen, Elliott D.
October 26, 1956
Primary view of Wing-Body Combinations With Wings of Very Low Aspect Ratio at Supersonic Speeds
Jorgensen, Leland H. & Katzen, Elliott D.
October 26, 1956
Primary view of Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models
Stone, David G.
May 26, 1950
Primary view of Wing-flow investigation of the characteristics of seven unswept, untapered airfoils of aspect ratio 8.0
Crane, Harold L. & Adams, James J.
June 13, 1951
Primary view of Wing-flow measurements of longitudinal stability and control characteristics of a canard airplane configuration with a 45 degree sweptback wing and a triangular all-movable control surface
Crane, Harold L. & Adams, James J.
August 25, 1950
Primary view of Wing-flow measurements of longitudinal stability and control characteristics of a supersonic airplane configuration having a 42.8 degree sweptback circular arc wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces
Crane, Harold L. & Adams, James J.
April 3, 1950
Primary view of Wing-Flow Study of Pressure-Drag Reduction at Transonic Speed by Projecting a Jet of Air From the Nose of a Prolate Spheroid of Fineness Ratio 6
Lopatoff, Mitchell
October 26, 1951
Primary view of Wing-flow tests of a triangular wing of aspect ratio two 1: effectiveness of several types of trailing-edge flaps on flat-plate models
Rathert, George A., Jr. & Cooper, George E.
November 14, 1947
Primary view of Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory
Rolls, L. Stewart & Matteson, Frederick H.
April 14, 1952
Primary view of Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
Robinson, Glenn H.; Cothren, George E., Jr. & Pembo, Chris
March 30, 1955
Primary view of Wing-load measurements of the Bell X-5 research airplane at a sweep angle of 58.7 degrees
Banner, Richard D.; Reed, Robert D. & Marcy, William L.
April 4, 1955
Primary view of Wing loads and load distributions throughout the lift range of the Douglas X-3 research airplane at transonic speeds
Keener, Earl R. & Jordan, Gareth H.
November 9, 1956
Primary view of Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds
Knapp, Ronald J. & Jordan, Gareth H.
November 4, 1953
Primary view of Wing-on and wing-off longitudinal characteristics of an airplane configuration having an thin unswept tapered wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4
Gillis, Clarence L. & Vitale, A. James
March 14, 1951
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Wing-Tunnel Investigation at High Subsonic Speeds of the Lateral-Control Characteristics of an Aileron and a Stepped Spoiler on a Wing With Leading Edge Swept Back 51.3 Degrees
Schneiter, Leslie E. & Hagerman, John R.
June 7, 1949
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