Add to ORKGDiscussed here are the aerodynamics of a subdivided wing section. The emphasis is upon the increase of lift with more acute angles of attack. Also discussed are wind tunnel tests of the relations among wind resistance, lift, angle of attack, and velocity
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
The following note, prepared for the NACA, contains several remarks on the possible improvement of t...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
These experiments were carried out to determine the aerodynamic characteristics of various triplanes...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, p...
The present report deals with a series of tests made for the purpose of improving flow conditions ab...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from t...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
The following note, prepared for the NACA, contains several remarks on the possible improvement of t...
In the subdivided wing section profile, the diagram of the current is entirely changed and the harmf...
These experiments were carried out to determine the aerodynamic characteristics of various triplanes...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, p...
The present report deals with a series of tests made for the purpose of improving flow conditions ab...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
The aerodynamic characteristics of seven unswept tapered wings were determined by calculation from t...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This investigation has a double object: 1) the calculation of the general characteristics of certain...