Download or read book The Use of Leading edge Area Suction to Increase the Maximum Lift Coefficient of a 35 Degrees Swept back Wing written by Curt A. Holzhauser and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Use of Leading edge Area Suction to Increase the Maximum Lift Coefficient of a 35 Degree Swept back Wing written by Curt A. Holzhauser and published by . This book was released on 1952 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Tests of a Leading edge Area Suction on a Fighter type Airplane with a 35 Degree Sweptback Wing written by Richard S. Bray and published by . This book was released on 1955 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a leading-edge area-suction boundary-layer-control system, and to investigate the possible operational limitations imposed on a fighter-type airplane by such an installation. The results of the flight tests are compared with those of full-scale wind-tunnel tests of a similar installation on a model incorporating F-86 wing panels. The basic porous-area distribution tested extended the full length of the wing leading edge. Suction power was provided by a modified turbosupercharger which was driven by air bled from the compressor of the airplane's jet engine.

Download or read book Wind tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 degree swept wing airplane written by Curt A. Holzhauser and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Note written by and published by . This book was released on 1964 with total page 1068 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Analysis of Wind tunnel Tests to a Mach Number of 0 90 of a Four engine Propeller driving Airplane Configuration Having a Wing with 40 Degrees Sweepback and an Aspect Ratio of 10 written by George G. Edwards and published by . This book was released on 1956 with total page 658 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted at speeds up to a Mach number of 0.90 to determine the effects of operating propellers on the longitudinal characteristics of a four-engine tractor airplane configuration having a 40 degrees swept wing with an aspect ratio of 10. Results of wind-tunnel tests of a model representing such an airplane configuration (see NACA TN 3789) show that these effects are of most concern in the low-speed high-thrust flight regime. In the present report the low-speed data are analyzed to determine the source of the various effects and to indicate how the adverse effects can be reduced, and the high-speed data are discussed primarily from the standpoint of Mach number effects. The analysis of the low-speed data indicates that the large variations of longitudinal stabil.itywith angle of attack resulted primarily from passage of the tail into and out of the slipstream. The slipstream also created large lift increments on the wing, particularly with flaps deflected, which resulted in increases in stability (with increasing thrust coefficient) from the outboard propeller and decreases in stability from the inboard propeller. It was concluded that the longitudinal stabiltty characteristics of the model couldbe improved by moving the nacelles outward, increasing the tail height, and reducing the tail span.

Download or read book The Use of Leading edge Area suction Flap to Delay Separation of Air Flow from the Leading Edge of a 35 Degrees Sweptback Wing written by Curt A. Holzhauser and published by . This book was released on 1954 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Use of a Leading edge Area suction Flap to Delay Separation of Air Flow from the Leading Edge of a 35 Degree Sweptback Wing written by Curt A. Holzhauser and published by . This book was released on 1953 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Factors Affecting the Maximum Lift drag Ratio at High Supersonic Speeds written by Charles H. McLellan and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.

Download or read book A Review of the Stall Characteristics of Swept Wings written by Charles W. Harper (Jr.) and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Use of Area Suction for the Purpose of Delaying Separation of Air Flow at the Leading Edge of a 63 Degrees Swept back Wing written by Woodrow L. Cook and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Theoretical Lift and Damping in Roll of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds written by Frank S. Malvestuto and published by . This book was released on 1949 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimation of the lift-curve slope and damping-in-roll derivative for given values of aspect ratio, taper ratio, Mach number, and leading edge sweep.

Download or read book Aeronautical Engineering Index written by and published by . This book was released on 1954 with total page 1212 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary layer Control for High Lift by Suction at the Leading edge of a 40 Deg Swept back Wing written by Great Britain Aeronautical Research Council and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerospace Engineering Index written by and published by . This book was released on 1959 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Preliminary Investigation of the Use of Circulation Control to Increase the Lift of a 45 Degree Sweptback Wing by Suction Through Trailing edge Slots written by Woodrow L. Cook and published by . This book was released on 1954 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary layer Control for High Lift by Suction at the Leading Edge of a 40 Deg Swept back Wing written by E. D. Poppleton and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: