UNT Libraries Government Documents Department - 5,163 Matching Results

This system will be undergoing maintenance January 24th 9:00-11:00AM CST.

Search Results

Primary view of Wing-tunnel investigation at low transonic speeds of the effects of number of wings on the lateral-control effectiveness of an RM-5 test vehicle
Johnson, Harold S
November 29, 1949
Primary view of Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body
Stivers, Louis S & Malick, Alexander W
February 2, 1950
Primary view of Wire cloth as porous material for transpiration-cooled walls
Eckert, E R G; Kinsler, Martin R & Cochran, Reeves B
November 13, 1951
Primary view of Yaw characteristics and sidewash angles of a 42 degree sweptback circular-arc wing with a fuselage and with leading-edge and split flaps at a Reynolds number of 5,300,000
Salmi, Reino J. & Fitzpatrick, James E.
December 10, 1947
Primary view of Yaw characteristics of a 52 degree sweptback wing of NACA 64(sub 1)-112 section with a fuselage and with leading-edge and split flaps at Reynolds numbers from 1.93 x 10(exp 6) to 6.00 x 10(exp 6)
Salmi, Reino J.
November 8, 1948
Primary view of Yawed-Landing Investigation of a Model of the Convair Y2-2 Airplane, TED No. NACA DE 363
Hoffman, Edward L. & Fisher, Lloyd J.
1951
Primary view of Zero-angle-of-attack performance of two-dimensional inlets near Mach number 3
Woollett, Richard R & Connors, James F
February 29, 1956
Primary view of Zero-lift drag of a large fuselage cavity and a partially submerged store on a 52.5 degree sweptback-wing-body configuration as determined from free-flight tests at Mach numbers of 0.7 to 1.53
Hoffman, Sherwood
February 26, 1957
Primary view of Zero-lift drag of a series of bomb shapes at Mach numbers from 0.60 to 1.10
Stoney, William E., Jr. & Royall, John F.
July 26, 1956
Primary view of The Zero-Lift Drag of Several Configurations of the XAAM-N-2 Pilotless Aircraft. TED No. NACA DE332
Hall, James R. & Sandahl, Carl A.
March 16, 1950
Primary view of Zero-lift drag of several conical and blunt nose shapes obtained in free flight at Mach numbers of 0.7 to 1.3
Piland, Robert O. & Putland, Leonard W.
March 23, 1954
Primary view of Zero-lift drag of the Chance Vought Regulus II missile at Mach numbers between 0.8 and 2.2 as determined from the flight tests of two 0.12-scale models: TED No. NACA AD 398
Church, James D.
July 27, 1954
Primary view of Zero-lift drag of the chance vought regulus it missile at mach numbers between 0.8 and 2.2 as determined from the flight tests of two 0.12-scale models
Church, James D.
July 15, 1954