An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a Mach number of 2.01

von Carlson, Harry W.
Veröffentlicht 1959

The lower bound of attainable sonic-boom overpressure and design methods of approaching this limit

von Carlson, Harry W.
Veröffentlicht 1962

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurement of the pressure fields of several wing-body combinations at a Mach number of 2...

von Carlson, Harry W.
Veröffentlicht 1961

Pressure distribution at mach number 2.05 on a series of highly swept arrow wings employing various degrees of twist and camber

von Carlson, Harry W.
Veröffentlicht 1962

Simplified sonic-boom prediction

von Carlson, Harry W.
Veröffentlicht 1978

A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic mach numers and large angles of attack

von Carlson, Harry W.
Veröffentlicht 1979

A wind-tunnel study of the applocability of far-field sonic-boom theory to the space shuttle orbiter

von Carlson, Harry W.
Veröffentlicht 1978

A study of the sonic-boom characteristics of a blunt body at mach number of 4.14

von Carlson, Harry W.
Veröffentlicht 1977

Estimation of leading-edge thrust for supersonic wings of arbitrary plabform

von Carlson, Harry W.
Veröffentlicht 1978

A numerical method for calculating near-field sonic-boom pressure signatures

von Middleton, Wilbur D.
Veröffentlicht 1965

Numerical methods for the design and analysis of wings at supersonic speeds

von Carlson, Harry W.
Veröffentlicht 1974

A study of the application of heat or force fields to the sonic-boom-minimization problem

von Miller, David S.
Veröffentlicht 1969

The shock-wave noise problem of supersonic aircraft in steady flight

von Maglieri, Domenic J.
Veröffentlicht 1959

Sonic-boom characteristics in the extreme near field of a complex airplane model at Mach numbers of 1.5, 1.8, and 2.5

von Morris, Odell A.
Veröffentlicht 1970

Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at mach numbers from 2.3 to 4.63

von Miller, David S.
Veröffentlicht 1971

Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds

von Carlson, Harry W.
Veröffentlicht 1979

A wind-tunnel investigation of the effect of body shape on sonic-boom pressure distributions

von Carlson, Harry W.
Veröffentlicht 1965

Sonic-boom characteristics of proposed supersonic and hypersonic airplanes

von MacLean, F. Edward
Veröffentlicht 1966

Application of sonic-boom minimization concepts in supersonic transport design

von Carlson, Harry W.
Veröffentlicht 1973

Supersonic wings with significant leading-edge thrust at cruise

von Robins, A. Warner
Veröffentlicht 1980