130+ 4,088 page 1950s Aircraft Airplane PROPELLER Aerodynamics Studies on CD for Sale

130+ 4,088 page 1950s Aircraft Airplane PROPELLER Aerodynamics Studies on CD For Sale

130+ 4,088 page 1950s Aircraft Airplane PROPELLER Aerodynamics Studies on CD:
$19.99

DIRECT DOWNLOADS AVAILABLE FOR PUBLICATIONS ONLY

Do you prefer a permanent digital download rather than a mailed physical CD/DVD? Request this by message to me with the CONTACT SELLER button and I will provide a permanent download link for all items and refund all shipping costs.

COMBINING SHIPPING COSTS

Are you purchasing multiple items? I will: a) combine all invoices before payment and charge shipping equivalent to one item, or b) refund all shipping costs in excess of one item after payment.

$3.00 first class shipping in U.S. and rest of world; save by combining sales. Over 100 pre-NASA publications through the 1950s dedicated to seaplane development and testing.

Just a SAMPLE of the CONTENTS:

John C Houbolt, George W Brooks; Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades; naca-report-1346; 1958

Albert J. Evans, George Liner; A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96; naca-report-1375; 1958

Max C. Kurbjun, Arthur W. Vogeley; Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72; naca-report-1377; 1958

Max C. Kurbjun; Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2; naca-tn-4172; Jan 1958

Kenneth P. Spreemann; Investigation of the effects of propeller diameter on the ability of a flapped wing, with and without boundary-layer control, to deflect a propeller slipstream downward for vertical take-off; naca-tn-4181; Dec 1957

William A. Newsom, Jr.; Experimental investigation of the lateral trim of a wing-propeller combination at angles of attack up to 90 degrees with all propellers turning in the same direction; naca-tn-4190; Jan 1958

Jerome B. Hammack, Thomas C. O'Bryan; Effect of advance ratio on flight performance of a modified supersonic propeller; naca-tn-4389; Sep 1958

William C. Hayes, Richard E. Kuhn, Irving R. Sherman; Effects of propeller position and overlap on the slipstream deflection characteristics of a wing-propeller; naca-tn-4404; SEP 1958

Thomas C. O'Bryan; Flight measurements of the vibratory stresses on a propeller designed for an advance ratio of 4.0 and a Mach number of 0.82; naca-tn-4410; SEP 1958

Robert T. Taylor; Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing; naca-tn-4126; Jan 1958

Thomas C. O'Bryan; Flight measurements of the vibratory bending and torsional stresses on a modified supersonic propeller for forward Mach numbers up to 0.95; naca-tn-4342; Jun 1958

James A. Weiberg, Roy N. Griffin, George L. Florman; Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and area-suction flaps; naca-tn-4365; Sep 1958

Max C. Kurbjun; Noise survey of a full-scale supersonic turbine-driven propeller under static conditions; naca-tn-4059; Jul 1957

Max C. Kurbjun; Effects of blade plan form on free-space oscillating pressures near propellers at flight Mach numbers to 0.72; naca-tn-4068; Aug 1957

Robert O. Schade; Flight-test investigation on the Langley control-line facility of a model of a propeller-driven tail-sitter-type vertical-take-off airplane with delta wing during rapid transitions; naca-tn-4070; Aug 1957

William A. Newsom, Jr; Effect of ground proximity on the aerodynamic characteristics of a four-engine vertical-take-off-and-landing transport-airplane model with tilting wing and propellers; naca-tn-4124; Oct 1957

Louis P. Tosti; Transition-flight investigation of a four-engine-transport vertical-take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream; naca-tn-4131; Dec 1957

Julian D. Maynard, Leland B. Salters, Jr.; Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers; naca-report-1309; Jan 1957

Robert M. Reynolds, Robert I. Samonds, John H. Walker; An investigation of single- and dual-rotation propellers at positive and negative thrust, and in combination with an NACA 1-series D-type cowling at Mach numbers up to 0.84; naca-report-1336; Jan 1957

Houbolt, John C Brooks, George W; Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades; naca-tn-3905; February 1957

Lovell, Powell M , Jr Parlett, Lysle P; Flight tests of a model of a high-wing transport vertical-take-off airplane with tilting wing and propellers and with jet controls at the rear of the fuselage for pitch and yaw control; naca-tn-3912; March 1957

Newsom, William A , Jr; Effect of propeller location and flap deflection on the aerodynamic characteristics of a wing-propeller combination for angles of attack from 0 degrees to 80 degrees; naca-tn-3917; 1957

Kuhn, Richard E Hayes, William C , Jr; Wind-tunnel investigation of effect of propeller slipstreams on aerodynamic characteristics of a wing equipped with a 50-percent-chord sliding flap and a 30-percent-chord slotted flap; naca-tn-3918; February 1957

Kuhn, Richard E; Investigation of effectiveness of a wing equipped with a 50-percent-chord sliding flap, a 30-percent-chord slotted flap, and a 30-percent-chord slat in deflecting propeller slipstreams downward for vertical take-off; naca-tn-3919; 1957

Hickey, David H.; Preliminary investigation of the characteristics of a two dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane; naca-rm-a57f03; 1957

Richard E. Kuhn, John W. Draper; Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees; naca-report-1263; Jan 1956

Vernon L. Rogallo, Paul F. Yaggy, John L. McCloud, III; An analysis of once-per-revolution oscillating aerodynamic thrust loads on single-rotation propellers on tractor airplanes at zero yaw; naca-report-1295; Jan 1956

Robert H. Kirby; Exploratory investigation of the effectiveness of biplane wings with large-chord double slotted flaps in redirecting a propeller slipstream downward for vertical take-off; naca-tn-3800; Oct 1956

Charles E. Watkins, Barbara J. Durling; A method for calculation of free-space sound pressures near a propeller in flight including considerations of the chordwise blade loading; naca-tn-3809; Nov 1956

Robert H. Kirby; Flight investigation of the stability and control characteristics of vertically rising airplane research model with swept or unswept wings and x- or +-tails; naca-tn-3812; Oct 1956

El Badrawy, Rashad M.; Flat plate cascades at supersonic speed; naca-tm-1369; 1956

Demele, Fred A., Kolbe, Carl D.; The effect of trailing-edge bluntness on the performance of a small-scale supersonic propeller at forward Mach numbers to 0.92; naca-rm-a55j12; 1956

Hickey, David H.; Full-scale wind-tunnel tests of the longitudinal stability and control characteristics of the XV-1 convertiplane in the autorotating flight range; naca-rm-a55k21a; 1956

Sammonds, Robert I Reynolds, Robert M; The pressure-recovery and propeller-force characteristics of a propeller-spinner-cowling combination employing NACA 4-(5) (05)-037 six- and eight-blade dual-rotation propellers with an NACA 1 series D-type cowl; naca-rm-a54j22; January 27, 1955

I. E. Garrick, Charles E. Watkins; A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers; naca-report-1198; 1954

W. H. Gray, J. M. Hallissy, Jr., A. R. Heath, Jr.; A wind-tunnel investigation of the effects of thrust-axis inclination on propeller first-order vibration; naca-report-1205; 1954

H. Clyde McLemore, Michael D. Cannon; Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees; naca-tn-3228; Jun 1954

Richard E. Kuhn, John W. Draper; An investigation of a wing-propeller configuration employing large-chord plain flaps and large-diameter propellers for low-speed flight and vertical take-off; naca-tn-3307; Dec 1954

Draper, John W Kuhn, Richard E; Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees; naca-tn-3304; November 1954

Sutton, Fred B Buell, Donald A; The effect of an operating propeller on the aerodynamic characteristics at high subsonic speeds of a model of a vertical-rising airplane having an unswept wing of aspect ratio 3; naca-rm-a52e06; November 15, 1954

Sutton, Fred B Demele, Fred A; The effects of operating propellers on the longitudinal characteristics at high subsonic speeds of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10; naca-rm-a53j23; January 07, 1954

Boltz, Frederick W Kolbe, Carl D; Effects of operating propellers on the wing-surface pressures of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback; naca-rm-a53l29; April 23, 1954

Reynolds, Robert M Molk, Ashley J; Effects of two spinner shapes on the pressure recovery in an NACA 1-series D-type cowl behind a three-blade propeller at Mach numbers up to 0.80; naca-rm-a53l29a; March 19, 1954

Demele, Fred A Otey, William R; Investigation of the normal force accompanying thrust-axis inclination of the NACA 1.167-(0)(03)-058 and the NACA 1.167-(0)(05)-058 three-blade propellers at forward Mach numbers to 0.90; naca-rm-a54d22; June 23, 1954

Reynolds, Robert M Walker, John H; Investigation of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at positive and negative thrust at Mach numbers up to 0.90, including some aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade, single-rotat; naca-rm-a54g13; October 08, 1954

Reynolds, Robert M., Kenyon, George C.; Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at Mach numbers up to 0.80; naca-rm-a54b18a; 1954

Rogallo, Vernon L., McCloud, John L., Yaggy, Paul F.; Note on the effects of first-order aerodynamic loads on propeller shaft loads with emphasis on counterrotating propellers; naca-rm-a54c30; 1954

Julian D. Maynard, Seymour Steinberg; The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65; naca-report-1126; 1953

William Solomon; Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller; naca-tn-2881; Jan 1953

Vernon L. Rogallo, John L. McCloud, III; Surveys of the flow fields at the propeller planes of six 40 degree sweptback wing-fuselage-nacelle combinations; naca-tn-2957; Jun 1953