|
|
1001.
|
Cyclic furnace oxidation of clad WI-52systems at 1040 degree and 1090 degree C [NASA TN D -6730]
by Gedwiil, , Michael A. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: 29p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1002.
|
An efficent algorithm using matrix methods to solve wind tunnel force balance [NASA TN D-686-79]
by Smith,David L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 43p.Publisher: Washington, D.C. National aeronautics and space administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1003.
|
Light detection electronics for a raman lidar [NASA TN D-6879]
by Leser,Robert J | Salzman,Jack A. Material type: Book Description: 27p.Publisher: Washington,D.C. National aeronautics and space administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1004.
|
Summary of design considerations for airplane spin recovery parachute systems
by Burk,Sanger M | Jr. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 53p.Publisher: Washington ;D. C. National aeronautics and space administration Availability: No items available
|
|
|
1005.
|
Summary of design considerations for airplane spin recovery parachute systems [NASA TN D -6866]
by Burk,Sanger M | Jr. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 53p.Publisher: Washington ;D. C. National aeronautics and space administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1006.
|
Spoked wheels to deploy large surfaces in spaces
: Weight estimates for solar arrays
by Crawford, R.F [etal.] | Hedgepeth, J.M. ,Preiswerk P.R. Material type: Book Description: 55p.Publisher: Washington, D.C National aeronautics and space administration 1975Availability: No items available
|
|
|
1007.
|
Analysis and calculation of lighting
: Induced voltages in aircraft electrical circuits
by Plunner,J.A | Plumer, J.A. Material type: Book Description: 57p.Publisher: Washington,D.C National aeronautics and space administration 1974Availability: No items available
|
|
|
1008.
|
Progreesof NASA resarch relatin to noise allleviaton of large subsonic jet aircrafft [NASA SP=189]
by Proceedings ... Conference held at large subsonc jet aircraft Hampton, Virgina 8-10, 1968. Material type: Book; Format:
print
; Literary form:
not fiction
Publisher: Washington, D C. National Aeronautics and Space Adminstration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1009.
|
Dynamic stability and dispersion of a project mercury test capsule upon entering the atmosphere , with effects of roll rate centre of gravity diplacement, and threshold of a rate reaction control system [NASA TM X-350]
by Jaquet, Byron M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 78p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1010.
|
An experimental study of the flutter of sails having a a delta planform tested from a macnh number of 0.1 to A mach number of 1.9 [NASA TM X-355]
by Hess, Robert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 39p.Publisher: Washington, D. C National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1011.
|
Wind tunnel investigationof the static and dynamicrotary stability derivativesofa fllat top wing body model at mach numbers of 2.5, 3.0 and 3.5 [NASA TM X-361]
by Lampkin, Bedford A | Endicott, Kenneth C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1012.
|
The effects of wing plan from on the the static longitudinal aerodynamic characteristics of a flat-top hypersonicaircraft at mach numbers from 0.6 to 1.4 [NASA TM X-364]
by Treon, Stuart L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1013.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing combinations of sonic design with diamond, delta and arrow plan from [NASA TM X-372]
by Holdway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1014.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing body combinations of sonic design with diamond delta and arrow plan forms [NASA TM X
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: No items available
|
|
|
1015.
|
Free flight measure
by Sommer, Simon C. Material type: Book Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1016.
|
Free flight measurements of static and dynamic stability of models of the project mercury re-entry capsule at mach numbers 3 and 9.5 [NASA TM X-373]
by Sommer, Simon C | Short, Barbara J | Compton, Dale L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1017.
|
Evaluation of blended wing body combinations with curved plan forms at mach numbersn uoto 3.50 [NASA TM X-379]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1018.
|
Experimental perfromance of area ratio 200,25 and 8 nozzles on JP-4 fuel and liquid oxygen rocket engine [NASA TM X-382]
by Lovell, Calvin Lowell | Lovell, J. Calvin, Samanich, Nick A. and Barnett, Donald O | Calvin, Lovell, J | Donald O,,Barnett. Material type: Book Description: 75p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1019.
|
Investigation at mach numbers of .60 to 3.50 of blended wing body combinationswith cambered and twisted wings with diamond, delta and arrow plan forms [NASA TM X-390]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
1020.
|
Heat transfer to blunt axially symmetric bodies [NASA TM X-391]
by Reller, John O. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
